1 2 3 4 5 CONCEPT OF OPERATIONS 6 (CONOPS) 7 FOR 8 9 INTERNATIONAL SPACE WEATHER INFORMATION 10 IN 11 SUPPORT OF INTERNATIONAL AIR NAVIGATION 12 13 14 15 16 17 18 19 20 21 September 2012 22 Version 2.0 23 Revision Date Description 0.1 2-15-2011 Initial International Oriented Draft 0.2 2-25-2011 Initial Internal FAA Comments 0.3 3-7-2011 Operational & Functional Matrix added & Outline adjustments made 0.4 3-18-2011 2nd round of internal FAA comments, added Figure 6 and 4 references in Appendix B, adjustments made to Figure 7, wording adjustments in many sections throughout document 0.5 3-23-2011 Merged content from Sections 2 and 3 were appropriate. Changed Section 4.2 Title, moved content at end of section to end of Forward 0.6 4-15-2011 Incorporated 314 Comments and significantly restructured the document, especially in for the Foreword, Introduction, first three sections, content structure for the Functional Requirements and added Appendices A-E 0.7 4-19-2011 Final Mature Draft – Added three additional Operational and Functional Requirements along with format spacing and some tweaks to the verbiage of several other Functional Requirements in section 5.2 0.8 5-17-2011 Incorporated comments of international task ad hoc group Member States & Organizations to meet Conclusion 5/19 from IAVWOPSG/5. Updated Figures 4 and 7 and Table 4a. 0.9 6-13-2011 Incorporated additional comments from international community received in late May and June 1.0 6-22-2011 Updated Figure 1, added a “Note” below Figure 7, 2nd round of document formatting and editing 2.0 9-28-2012 Adjudicated and thoroughly addressed over 800 global comments. Incorporated at least part of each of the overwhelming majority of comments. There was a recent new requirement to follow a new outline for all Concept of Operations documents and therefore, the format and infrastructure of the document was overhauled. 24 TABLE OF CONTENTS 25 26 1 Introduction ......................................................................................................... 1 27 1.1 Background ...................................................................................................................... 1 28 1.2 Problem Statement ........................................................................................................... 3 29 1.3 Identification .................................................................................................................... 3 30 1.3.1 Operational User Need for Space Weather Aviation Services ................................. 3 31 1.3.2 User Need for Aviation-Specific Space Weather Information ................................. 4 32 1.3.3 Impacts of Space Weather on Aircraft Operations ................................................... 4 33 1.3.3.1 Communications ................................................................................................ 4 34 1.3.3.2 Navigation .......................................................................................................... 5 35 36 1.4 2 37 Concept Overview ............................................................................................................ 7 Current Operations and Capabilities ................................................................... 9 2.1 Description of Current Operations ................................................................................... 9 38 2.1.1 Observations ............................................................................................................. 9 39 2.1.2 Analysis................................................................................................................... 10 40 2.1.3 Forecasts ................................................................................................................. 11 41 2.2 42 Current Supporting Infrastructure for Space Weather Products and Services ................ 11 2.2.1 Current Supporting Infrastructure from International Organizations ..................... 13 43 2.2.1.1 International Civil Aviation Organization ........................................................ 13 44 2.2.1.2 World Meteorological Organization ................................................................ 13 45 2.2.1.3 International Space Environment Service ....................................................... 13 46 2.2.1.3.1 Regional Warning Centers ............................................................................. 13 47 2.2.1.3.2 The NOAA Space Weather Prediction Center ............................................... 14 48 2.2.1.3.3 Australian Space Weather Information Services ........................................... 15 49 3 50 Description of Changes ..................................................................................... 15 3.1 Proposed Service Description ........................................................................................ 17 51 3.1.1 Standardizing Aviation Space Weather Information .............................................. 17 52 3.1.2 Integration and Delivery of Space Weather Meteorological Services .................... 22 53 54 4 Proposed Concept.............................................................................................. 23 4.1 Assumptions and Constraints ......................................................................................... 23 55 4.1.1 Assumptions for Airline Industry Operations ......................................................... 23 56 4.1.2 Constraints to Providing Robust Space Weather Products and Services ................ 23 i 57 4.2 Operational Environment ............................................................................................... 23 58 4.3 Operations ...................................................................................................................... 27 59 4.3.1 Existing and Future Space Weather Information .................................................... 27 60 4.3.2 Future Targets for Outlook Information ................................................................. 28 61 4.4 Operational Requirements .............................................................................................. 30 62 4.5 Supporting Infrastructure ............................................................................................... 31 63 4.6 Science Benefits to Be Realized .................................................................................... 34 64 4.7 Cost Benefits Associated with Polar Routes .................................................................. 34 65 5 Space Weather Requirements for Aviation....................................................... 35 66 5.1 Functional Requirements ............................................................................................... 35 67 5.2 Performance Requirements ............................................................................................ 35 68 5.2.1 Existing Performance Requirements....................................................................... 35 69 5.2.2 New Performance Requirements ............................................................................ 35 70 6 Operational Scenario ......................................................................................... 36 71 7 Summary of Impacts ......................................................................................... 38 72 APPENDIX A: Material List of References ............................................................................... A-1 73 APPENDIX B: Definitions ......................................................................................................... B-1 74 APPENDIX C: Functional and Performance Requirements ...................................................... C-1 75 APPENDIX D: Space Weather Impacts on Aviation ................................................................. D-1 76 APPENDIX E: Space Weather Alert and Forecast Products.......................................................E-1 77 APPENDIX F: Delineating Regions of Space Weather Impact .................................................. F-1 78 APPENDIX G: Bi-Lateral Agreements ...................................................................................... G-1 79 APPENDIX H: Introduction to Space Weather .......................................................................... H-1 80 81 ii 82 LIST OF FIGURES 83 Figure 1: Polar Routes Necessitate HF Radio Communications at High Latitudes. ...................... 6 84 85 Figure 2: Total Traffic Density for Northern Cross-polar Routes 2000-2011 Sources: NAVCANADA and United Airlines .............................................................................................. 7 86 Figure 3: Global Space Weather Service Perform These Functions............................................... 8 87 88 Figure 4: The RWC in Boulder has a Special Role in the “World Warning Agency,” Acting as a Hub for Data Exchange and Forecasts. ...................................................................... 14 89 Figure 5: Future Production and Communications Concept......................................................... 26 90 Figure 6: Phases of Flight ............................................................................................................. 36 91 Figure 7: Ladder Sequence Diagram Showing How Operational Scenarios are Depicted........... 37 92 Figure 8: Convective Weather Impact Mitigation Process ......................................................... B-1 93 Figure 9: The Time Scales of Solar Effects (Source: NOAA SWPC) ........................................ D-7 94 95 Figure 10: Magnetic Latitudes Already Established for Magnetic Observatories Around the World ........................................................................................................................ F-2 96 97 98 99 LIST OF TABLES 100 Table 1: NOAA Space Weather Scale for Radio Blackout Events .............................................. 19 101 Table 2: NOAA Space Weather Storm Scale for Radiation Storm Events .................................. 20 102 Table 3: NOAA Space Weather Storm Scale for Geomagnetic Storm Events............................. 21 103 Table 4: User Needs to Better Understand and Mitigate SWx Impacts on Aviation Operations . 24 104 Table 5: Summary of General (%) Confidence Levels in Future Forecast Products.................... 29 105 Table 6: Aviation User Need Statements ...................................................................................... 31 106 Table 7: SWx Information versus Decision-maker Matrices ....................................................... 33 107 Table 8: Reference List ............................................................................................................... A-1 108 iii 109 1 110 Scope 111 112 113 114 115 116 117 118 This Concept of Operations (ConOps) document describes the potential impact of Space Weather (SWx) on aviation operations, the current provision of SWx information to support aviation decision-makers, and the future concept and environment for the use of SWx information. SWx information includes observations, analyses, and forecasts. Aviation decision-makers use SWx information for flight planning and en route deviations. This requires knowledge, guidelines, and information to support risk management processes within the aviation industry. This document provides a global approach to the provision of SWx information. It conveys how SWx information can be globally-harmonized and integrated into aviation decision-making processes. 119 120 121 122 123 124 This ConOps communicates the overall requirements for SWx information to meet the operational needs of various aviation decision-makers. This document describes the operational, functional, and performance requirements for SWx information to support international air navigation. The expectation is that the ConOps will evolve as scientific improvements in forecasting events improve and the effects of SWx on communications, navigation, and surveillance systems are better understood. 125 126 127 128 This document addresses the impacts of elevated radiation levels on avionics equipment. It does not address the possible adverse effects of exposure to elevated radiation levels on human health. Establishing requirements for cumulative dosage rates is beyond the purview of the International Airways Volcanic Watch Operations Group (IAVWOPSG). 129 1.1 130 INTRODUCTION Background Purpose 131 132 133 134 135 136 137 138 139 The purpose of the ConOps is to define the requirements for the provision of SWx information based on the intended use of that information to support air navigation. It identifies the types of SWx information needed to mitigate hazards caused by solar events. These hazards can include degraded avionics, degraded or disrupted communications, and navigation, and increased radiation exposure. Although SWx impacts are global in nature, the impacts are most prevalent in the Polar Regions. This document presents an initial set of operational, functional, and performance requirements for acceptance by the International Civil Aviation Organization (ICAO). The intent is to achieve global harmonization through a set of global standards for SWx information. 140 141 142 143 144 145 146 147 148 149 150 The ionosphere is made up of a rarified plasma zone that begins at an altitude of approximately 50 km above the Earth, is a critical medium for aviation High Frequency (HF) communications. When its total electron density is perturbed by effects from space due to energy inputs from the active Sun, or when intense convective terrestrial weather from the troposphere below perturbs the ionosphere, the HF signal can be attenuated or absorbed. This can cause the signal to disappear entirely, or diminish to an unusable, faded signal. Depending on the amount of ionization present, radio signals interacting with the ionosphere may suffer losses (weaken) in a process called absorption. Imagine the ionosphere to be a set of louvers. Degradation of HF communications due to absorption is most significant when the lower ionosphere composition is effected by solar weather events, closing the louvers. If the ionosphere is “quiet,” the louvers are fully-open and the signal pass through easily. 1 151 152 153 154 155 156 157 158 159 160 161 Future Air Traffic Control (ATC) systems will be based primarily on the space-based Global Navigation Satellite System (GNSS). Satellite technology is a foundation for both the US Next Generation Air Transportation System (NextGen) and Europe’s Single European Sky Air Traffic Management Research (SESAR). Therefore, any limitations or outages of the satellite systems must be considered during flight planning and en route operations. Solar events can affect flight operations by disrupting communications, navigation, and positioning capabilities and endangering human health. The SWx events of greatest concern to aviation operations are those that disrupt the operational systems and increase the radiation environment: Galactic Cosmic Rays (GCR), Solar Energetic Particles (SEP), Coronal Mass Ejections (CME) and Geomagnetic Storms (and more directly, the ionospheric disturbances). The impacts are most acute in the Polar Regions. Aviation decision-makers need timely and accurate forecasts for these SWx events. 162 163 164 165 166 167 168 169 170 SWx already adversely affects aircraft communication, navigation, and positioning systems, across many parts of the globe. Satellite-based navigation using GPS receivers operating on the dayside of the Earth can be impacted over the mid-latitudes. Radio blackouts primarily affecting HF communication frequencies are a consequence of enhanced electron densities caused by emissions from solar flares that ionize the sunlit side of the Earth.1 Radiation exposure risk is greatest over the poles, and lessens at lower latitudes. Observing, forecasting, and disseminating information about the space environment is critical to aviation operations today, and it will be even more important as the use of Reusable Launch Vehicles (RLV) in suborbital altitudes increases in the near term (~2013). 171 Objective 172 The following summary reinforces the objectives of this ConOps: 173 174 175 176 177 178 179 Why? Most SWx effects are global in nature. SWx phenomena affect aviation operations (especially polar flights), degrading efficiency and elevating safety concerns for crew and passengers. ICAO does not currently include requirements for SWx in its recommended meteorological information. SWx impacts on aviation operations, particularly long-haul polar routes, are increasingly a recognized part of the overall industry operating costs. As the number of these types of flights continues to increase, the fiscal consequences of delays or diversions grows. 180 181 182 183 184 185 Who? The operator is the user of SWx products (The operator is a person, organization or enterprise engaged in or offering to engage in an aircraft operation.). The avoidance of SWx event situations en route is the responsibility of the flight crew and those responsible for operational control of a flight. Flight Operations Centers (FOCs) try to minimize the effects of solar events through pre-flight planning. Air Traffic Services assist flight crew members in avoiding/reducing the impacts of SWx events on flight operations. 186 187 188 How? This document describes the operational concepts to mitigate impacts of SWx on aviation operations. This will be accomplished through the establishment of global standards for the provision and use of SWx information. The SWx information includes the following: 189 190 Remote Sensing helping to analyze and determine the severity of the impact on various operational services. 1 NOAA, Space Weather Prediction Center (SWPC), Manual on Space Weather Effects in Regard to International Air Navigation (January 2011). 2 191 192 In Situ Observations from many space-based and some ground-based monitoring systems to determined when solar flares occur. 193 194 Nowcasts/Forecasts predict when eruptions from the Sun will interact with the Earth’s atmosphere. 195 196 197 198 199 Lastly but certainly not least important, an operator’s internal Safety Management System (SMS), Safety Risk Assessment (SRA) processes take precedence over all other processes and will be described. 200 201 202 203 SWx impact on aviation needs more reliable forecasting with greater lead-times and higher confidence levels in order to increase global harmonization of information dissemination processes and operations. This document looks at concepts attempting to mitigate aviation operational impacts caused by various SWx phenomena on communications and navigation. 204 Communications 205 Problem 1: SWx can negatively affect aircraft communications. 206 Impact: Lost or significantly degraded quality of continuous communications. 207 Navigation 208 Problem 2: SWx can negatively affect satellite-based navigation systems. 209 210 211 212 213 Impact: The Wide Area Augmentation System (WAAS) and the European Geostationary Navigation Overlay Service (EGNOS) and the other ground-based augmentation systems can be degraded to the point that its vertical guidance approach protection limit can be compromised, and en route avionic equipage readings can become erroneous. In addition, some aspects of or all of GNSS may be affected to some degree if the ionosphere is perturbed. 214 Radiation 215 Problem 3: SWx can negatively affect the performance of avionics systems. 216 217 218 219 220 221 Impact: Radiation exposure can affect installed and handheld avionics equipage. A summary of conceptual steps will be defined in the following sections, which identify user needs, to include the unallocated operational functional requirements. This process allows for the analysis of SWx observational data to be utilized more effectively through Decision Support Tools (DST) then perhaps information retrieved at face-value by SWx service providers refining planned or ongoing operational scenarios. 222 223 1.3 224 1.3.1 Operational User Need for Space Weather Aviation Services 225 226 227 228 229 230 231 232 Use of polar flight routes creates efficiencies in air travel by vastly reducing travel distances and required fuel (Figure 1). As Figure 2 shows, airlines are increasingly relying on those polar routes, necessitating accurate and timely observation and forecasting of SWx to mitigate impacts on aviation industry operations, on which global economies depend. SWx adversely affects aviation operations through the loss of communication and navigation, and negative health effects on passengers and crew. Though these impacts are more prevalent over the Polar Regions, their impacts on communications, navigation, and radiation exposure extend in various degrees to other parts of the globe and to other applications. 1.2 Problem Statement Identification 3 233 234 235 236 237 238 1.3.2 User Need for Aviation-Specific Space Weather Information Specific SWx information was gathered from a number of sources by various means, including recommendations, guidance material, and workshops/working groups led by subject matter experts. An initial consensus was reached at the last joint World Meteorological Organization (WMO) and ICAO Divisional Meeting in 2002, which stated the need to consider SWx a hazardous impact to aviation operations. 239 240 241 242 243 244 245 246 247 248 249 250 As part of a Policy Program Study, the American Meteorological Society (AMS) and SolarMetrics through the ad hoc The Cross Polar Trans East Air Traffic Management Providers Working Group (referred to as the CPWG), published a policy workshop report in March 2007 on “Integrating Space Weather Observations and Forecasts into Aviation Operations.” This report recommended that “the aviation industry needs to clearly define its requirements for space weather information and how it is incorporated into the operational decision making process.” A sub-group of the CPWG was selected to lead the process for defining these user service needs. The CPWG provides a forum for Air Navigation Service Providers (ANSP) and operators to meet and explore solutions for improving air traffic services to aircraft that operate between North America and Asia via Cross Polar and Russian Trans East routes. The CPWG established a SWx sub-group to focus on aviation SWx user service needs, and the aforementioned task force focused on SWx issues.2 251 252 253 254 255 The IAVWOPSG noted at its fourth meeting in Paris in September 2008 that there was not yet a complete understanding among the user community of SWx products and information that could be helpful in support to them of their operational decisions. The IAVWOPSG agreed to formulate Conclusion 4/29, a directive to develop SWx training guidance material before formally introducing aviation requirements related to SWx. 256 1.3.3 Impacts of Space Weather on Aircraft Operations 257 258 259 260 261 The operator’s responsibility for safe and economical operations depends on accurate and timely forecasting for effective decision making. Critical to this process is the efficient information transfer from the forecaster to the decision-makers: operators, flight crew members, air traffic services, and government agencies. The variability of SWx event duration, frequency, and severity makes forecast accuracy and its timing information critical. 262 1.3.3.1 Communications 263 264 265 266 267 268 269 270 271 SWx events can impair communication systems by perturbing the ionosphere, which is a key part to HF communications for aviation. HF frequencies need the ionosphere to reflect the signal back to the Earth. All communications with en route aircraft poleward of 78No and 60So latitude can be lost during a disruptive SWx event. The hemispheric latitudes are different is because 60So is based on the vast open distances in the southern hemisphere, over which aircraft fly that have other issues beyond being able to see geostationary satellites. It was a purely a practical operational choice. For satellite communications, the higher frequencies that must pass through the ionosphere in order to allow for satellite communications may suffer loss of power or frequency stability. 272 273 274 275 As flight paths venture poleward, they lose their communication link with the geosynchronous communication satellites due to the Earth’s curvature, and conventional HF radio communication must be employed. Solar storms can render HF communications inoperable for periods of minutes, hours or even several days at a time. These disruptions in the ionosphere’s electron 2 Space Weather Sub-Group of the Cross Polar Working Group, “Integrating Space Weather Observations & Forecasts into Aviation Operations, Aviation Space Weather User Requirements,” Version 3.02 (November 2010). 4 276 277 278 279 280 281 282 283 284 285 density can occur to the point that radio signals can no longer be bounced back to the aircraft, and are driven by the size and location of the disturbance on the Sun that triggers these events. When communication disruptions at high latitudes occur along the limited polar routes, additional cost or delay can be introduced as air traffic controllers reduce air traffic flow rates by increasing the separation distances between aircraft flying at similar altitudes. This necessary safety precaution often reduces the overall aviation industry efficiency and capacity along polar routes, affecting profit margins for the airlines. There are polar orbiting Iridium spacecraft that offer L-band communication frequencies for additional cost, and that partially fill this communication gap. But as of today, most airlines are not currently equipped to take advantage of that capability. 286 287 288 289 290 Furthermore, there are both international recommendations and civil aviation authority requirements (see below) that communication be of good quality and take place continuously. Therefore, it is imperative that observations, forecasts, and SWx alerts and warnings be provided to the crew in order to mitigate potential problems with radio HF and satellite communications. Reliable communications are a vital component of safe and efficient air travel. 291 292 The following recommendation (not a requirement) from ICAO Annex 11 describes the importance of international flight communications:3 293 294 Whenever practicable, air-ground communication facilities for flight information service should permit direct, rapid, continuous and static-free two-way communications. 295 296 It is clear from excerpts within the ICAO Annex 2, that reliable communication is required at all times for aircraft on controlled flights:4 297 298 For two-way communication either possible according to paragraph 3.6.5.1, or communications failure rules according to paragraph 3.6.5.2 have to be followed. 299 300 There are current FAA requirements for domestic airline flight communications (crucial for passing weather information).5 301 302 303 § 121.99 Requires reliable and rapid communication over the entire route between the airplane and the appropriate dispatch office and between each airplane and the appropriate air traffic control unit. 304 1.3.3.2 Navigation 305 306 307 308 309 310 311 Satellite-based navigation can be affected at all latitudes, but occurs with more frequency at or near the poles and equator. SWx activity has disrupted the FAA’s WAAS by degrading its ability to provide vertical guidance protection limit for time periods of many hours to more than half a day.6 Satellite-based navigation is a key element in performance-based navigation as part of the global Air Traffic Management (ATM) concept. The implementation planned for NextGen and SESAR is in support of global ATM. Thus the need to monitor and predict SWx is more important than ever. 3 ICAO Annex 11, Chapter 6, Air Traffic Services Requirements for Communications, paragraph 6.1.2.2. ICAO Annex 2, Rules of the Air, To the Convention on International Civil Aviation, Chapter 3, Ninth Edition (July 1990). 4 5 Code of Federal Regulations (CFR) Title 14 (Aeronautics and Space). Report of the Assessment Committee for the National Space Weather Program, FCM-R24-2006, Office of the Federal Coordinator for Meteorological Services and Supporting Research (OFCM) (June 2006). 6 5 UAL POLAR ROUTES WASHINGTON 82 N PIRE L CHICAGO MAGUN ABERI NALIM DEVID RAMEL NIKIN ORVIT BEIJING HONG KONG SHANGHAI TOKYO 312 313 Figure 1: Polar Routes Necessitate HF Radio Communications at High Latitudes.7 314 315 Using polar routes necessitates HF radio communications at high latitudes (circular area in Figure 1). However, they are frequently disrupted by SWx events. 316 317 Figure 2 depicts the dramatic growth in cross-polar flights leading to increased aviation industry vulnerabilities. 7 Michael Stills, United Airlines, “Polar Operations and Space Weather,” presentation to the space weather enterprise forum, (June 21, 2011). 6 2000 7999 6357 5308 3731 2053 776 841 884 402 0 318 319 320 1 000 2 000 3 000 4 000 5 000 6 000 Figure 2: Total Traffic Density for Northern Cross-polar Routes 2000-20118 Sources: NAVCANADA and United Airlines 321 1.4 Concept Overview 322 323 324 325 326 327 A SWx service provides SWx information and/or products to the user. This service would include acquired or input data and interfaces across any existing or new implemented system. Services are defined in terms of the information they present. A SWx system, on the other hand, produces or generates SWx information or products, to be disseminated to the user, or another system. Global Space Weather Service requirements will be allocated to provider services, who then allocate requirements to weather systems. 8 Michael Stills, United Airlines, in support of FAA Concept of Operations for International SWx Information, presentation at the AMS 9th Symposium on SWx (January 2012). 7 7 000 328 329 330 331 332 333 334 The objective of a SWx service is to provide information to the global community relating to SWx conditions that may adversely affect communications, navigation, equipment, or humans. This information is of the following types: a. Space Weather Observation Information Information c. Space Weather Forecast Information b. Space Weather Climatology d. Space Weather Analysis Information Hierarchy Global Space Weather Service Observation Service Climatology Service Sample Requirement Operational What Must Be Done Global Space Weather Service Operational What Must Be Done Space Weather Service Space Weather Service shall provide forecasts for space weather Functional What Data Is Produced Space Weather System Space Weather Service shall generate space weather forecasts The GSWS shall provide space weather forecasts Forecast Service Analysis Service 335 336 Figure 3: Global Space Weather Service Perform These Functions 337 It is important to establish a distinction between operational and functional requirements. 338 339 340 The operational requirements are high-level requirements that define what must be done, are written from the operator’s perspective, and constitute what operations must do to provide the SWx service. 341 342 The high-level functional requirements describe the information to be produced or generated/ integrated by a generic, implementation-independent SWx system. 343 A proposed SWx Service would present the following standardized SWx information: 344 1. Standardized Index Thresholds 345 2. Standardized Space Weather Impact Indicator 346 3. Standardized Space Weather Information 347 348 349 350 351 352 353 354 355 356 357 Areas of the world experiencing similar SWx effects can be much larger than those of any Meteorological Watch Office (MWO). In order to avoid duplication of effort and possible confusion and conflicting information, it will be advantageous to consolidate the responsibilities of the MWOs, with regard to SWx, into a to-be-determined number of Space Weather Watch Offices, similar to the the International Space Environmental Service’s (ISES) 14 Regional Warning Centers (RWC). Whatever the number of centers chosen, there is a clear need for standards in geographic and technical aspects of SWx information and warnings for aviation with global scope. ISES and the RWCs would need to coordinate closely on the issuance of SWx information impact aviation. It’s also important to keep in mind that it could be some time before products with the level of details requiring graphical and gridded presentation are available to meet user needs. Therefore, consideration should be given to include textual/non-graphical 8 358 359 360 361 362 363 364 365 366 products as an official product in Annex 3 for the near term.9 That notwithstanding, the information should be disseminated along the lines of the present tropical cyclone and other unique terrestrial weather event warnings to meteorological authorities for dissemination locally to airlines under regional agreements. The means of communication might be similar to the World Area Forecast Satellite Broadcast System (WAFS) or the Aeronautical Message Handling System (AMHS),10 written in normal meteorological terminology and formatted for users for inclusion in flight plan packages and briefings. ICAO and WMO will need to continue to work together in order to achieve these fundamental principles that the provision of SWx information is an operational requirement. 367 2 368 2.1 369 370 371 372 373 374 375 376 377 378 379 The following types of SWx information are required for aircraft operations: observations, analyses, and forecasts. As with terrestrial weather, SWx data are obtained via both ground and space-based instruments. These instruments give forecasters the best assessment of current SWx conditions to help better understand and predict potential impacts from SWx activities. These measurements provide insight into the spatial and temporal complexity of the magnetic field lines of the magnetosphere and electron densities of the ionosphere that impact aviation operations in various ways. The data are then output as alerts, warnings, and forecasts for given SWx elements known to impact satellite and aviation operations. The intent of this ConOps is to convey how SWx alerts and warnings need to become a mainstay of global harmonization in airline operations. The SWx specification and forecast services require four strategic elements: observations, data access and display, predictions, and product dissemination. 380 2.1.1 Observations 381 382 383 384 385 386 387 388 389 390 391 392 393 394 395 396 397 398 399 Observations are classified as data measured by sensors. The suite of instruments that monitor SWx data collects ground-based, airborne, and/or space-based observations. These SWx observations allow the characterization of the spherical space region (Sun-Earth, also known as the heliosphere, see Appendix B for details), that is 1016 times greater than the spherical shell of the troposphere around the Earth. An example observation platform would be the U.S. Geostationary Operational Environmental Satellite (GOES) satellite, whose X-ray peak brightness is aligned by class and by energy flux to the National Oceanic and Atmospheric Administration (NOAA) SWx Radio Blackout Scales. GOES also makes high-energy particle flux measurements averaged in five-minute increments to define the NOAA Space Weather Radiation Storm Scale intensities (S-scale). The Solar Terrestrial Relations Observatory (STEREO) satellite is another observation platform that detects the Sun’s eruptions, and enables a full 3-D analysis of the eruption. The goal of the Solar Dynamics Observatory (SDO) is to understand the Sun's influence on Earth and near-Earth space. SDO will investigate how the Sun’s magnetic field is generated and structured, how this stored magnetic energy is converted and released in the form of solar wind, energetic particles, and variations in the solar irradiance. The Advanced Composition Explorer (ACE) satellite, positioned along the Sun-Earth line at the equilibrium gravitational point, the so-called L1 point, one and one-half million miles kilometers from the Earth, is the only deep SWx monitor station (similar to a terrestrial surface weather observation station) providing in situ measurements of highly-charged particles in the CURRENT OPERATIONS AND CAPABILITIES Description of Current Operations 9 ICAO Annex 3, “World Area International Air Navigation,” Chapter 3, Meteorological Watch Offices, 16th Edition (July 2007). 10 ICAO Annex 10, Aeronautical Telecommunications, Chapter 4, Aeronautical Fixed Services, 6 th Edition (October 2001). 9 400 401 402 403 404 405 solar wind moving directly at the Earth’s magnetosphere. In the U.S., data is gathered through a suite of observation platforms that include a network of ground-based magnetometers, spacebased solar telescopes, satellites, ionosondes, radio telescopes and GPS receivers. GPS receivers collect ionospheric data. The ionosphere is perturbed by effects of the solar wind that often degrades aviation radio communications. These are just a sample of capabilities used today, and those needed to support the airline service requirements. 406 407 408 409 410 411 412 413 414 415 416 417 418 Collating this array of SWx data can provide additional insight to the spatial and temporal electron density structure in the ionosphere that can cause scintillation on the L-band (GPS) radio frequency communications. At the same time, there has been the prospect of flying radiationmeasuring instruments (dosimeters) on aircraft or RLVs to routinely quantify the radiation dose impacts to better understand the radiation environment at aircraft altitudes. In fact, dosimeters are currently located on the International Space Station. This will help quantify the radiation in a given area, and can lead to improved understanding of the radiation environment at aircraft, suborbital, and low-Earth orbit altitudes. In addition, these measurements help validate some radiation models and tools, like Nowcast of Atmospheric Ionizing Radiation for Aviation Safety (NAIRAS) (See Appendix B).11 Aircraft observations from pilots (i.e., AIREPs or PIREPs) could improve the understanding of SWx event nuances related to onboard impacts by reporting communication difficulties (including presence or Northern/Southern lights) and suspicious or erroneous avionics measurements (navigation). 419 420 421 422 423 424 425 Observations from space assets provide data which supports substantially improved forecasts. Both the Solar and Heliospheric Observatory (SOHO) spacecraft and the ACE spacecraft are located at an L1 orbit. ACE provides crucial short-term warnings with very high confidence for the onset of major geomagnetic and radiation storms. SOHO provides observations of CMEs that provide a 1-3 day advanced warning of geomagnetic storms. The pair of STEREO spacecraft (A and B, leading and trailing Earth in its orbit) provided CME measurements in 3-D visual stereo images that lend much insight into the physical properties of coronal eruptions. 426 2.1.2 Analysis 427 428 429 430 431 432 433 434 435 436 437 438 439 440 A SWx analysis capability analyzes the potential, severity, or other aspects of a solar storm event. Analysis of SWx information can be difficult because of its scarcity. Proper interpretation of observed SWx data is the necessary precursor to reliable and enhanced forecast products. But unlike most hazardous terrestrial weather, SWx events occur on a time scale comparable to tornado warnings and micro-bursts. On average, lead-times are 30 minutes or less. Extending these lead-times is paramount to mitigate the severity of impact to safety, operations, and cost. Unfortunately, there are no ground-truth measurements that can be used to initialize a forecast until the elements of a solar storm are already 99 percent of the way toward Earth. The WMO Statement of Guidance on Space Weather Observation12 states the “vastness of space and the wide range of physical scales that control the dynamics of SWx demand that numerical models be employed to characterize the conditions in space to predict the occurrence and consequences of disturbances. Data assimilation techniques must be utilized to obtain the maximum benefit from more coarse measurements, SWx observations are therefore used through data assimilation into empirical or physic-based models.” 11 Prototype operational model that will provide a tool for commercial airlines and aircrew to monitor current and accumulated radiation exposure, under development at NASA Langley Research Center. 12 WMO Space Programme SP-5, The Potential Role of WMO in Space Weather (April 2008). 10 441 2.1.3 Forecasts 442 443 444 445 446 447 448 449 450 SWx forecasts give probabilistic estimates of the eruptive conditions at the Sun, as well as geophysical conditions nearer earth, that impact aviation operations. Characterization and/or predictions of the space environment from the Sun to the Earth’s surface are based upon observational data that monitor the Sun, and its sunspots. When a solar flare and/or CME occur, this data is input into the space-physics mathematical and empirical models to determine the impacts to orbiting spacecraft, communication, navigation, and other Earth-related impacts to those users operating in the near-Earth environment and dependent on space-based technology. These multi-dimensional forecast problems must meet current aviation operator needs (Table 6). Some samples of forecast products available from the SPWC website are shown in Appendix F. 451 452 453 454 455 456 457 458 459 460 461 462 463 464 465 466 467 Photons projected from the Sun’s surface as a result of magnetic field eruptions travel at the speed of light and cause HF dayside aviation communications blackouts with no lead time. Similar to the analysis challenges of forecasting terrestrial weather events related to tornadoes or micro-bursts, it is a challenge to disseminate information on this SWx hazard to aviation operations in a timely manner. Even solar winds associated with solar storms carry highlycharged particles traveling at million(s) of miles per hour (much slower than speed of light) through deep space, which, at times, slam into the Earth’s magnetosphere, doing so with little advance notice in some cases. CME events generally occur on timescales more typical of synoptic scale terrestrial forecasting (20 hours to four days). In one aspect, the timescales for geomagnetic-type storm forecasting SWx impacts generally compared to some terrestrial hazardous weather event movements, though the impacts are usually quite different. Interference and disruption of telecommunication frequencies necessary to maintain aviation communication and navigation integrity occur in rapid fashion across the scale of hemispheric regions and a multitude of Flight Information Regions (FIR), lasting from minutes to hours, sometimes stretching days in duration. Therefore, unlike terrestrial weather in-flight advisories, the format used for displaying impact information of SWx on aviation may or may not be an appropriate means of dissemination. 468 469 timescales generally for forecasting SWx impacts compared to terrestrial hazardous weather event movements are quite similar 470 471 472 473 474 Therefore, the goal is to improve the reliability and confidence levels with in-flight SWx advisories. This can be accomplished through better methods of monitoring and sensing observational measurements that feed into improved physics-based and/or empirical-based models supporting SWx forecast products. 475 2.2 476 477 478 479 480 SWx products and services are primarily available from state-sponsored international organizations as a part of the global effort for harmonization of SWx information into a single standard. Products and services being considered must be adequate for use in both the northern and southern polar region. If a case exists where this uniformity cannot be extended to both regions, regardless of the reason, a different level of service or product must be provided. 481 482 483 484 485 As in the case of terrestrial weather, reliable SWx information and forecasts are available from commercial providers in addition to state-sponsored services. These commercial services would render beneficial support in the form of tailored-made, value-added, rapid, and continuous SWx information and forecasts. These services would be critical for pre-flight pilot briefings, enroute updates, and for appropriate dispatch offices, etc., in accordance with established standards. The Current Supporting Infrastructure for Space Weather Products and Services 11 486 487 commercial providers could also provide their customized products as adjunct to near-real time SWx warnings, alerts, update messages, and post-event analysis. 488 489 490 491 Since SWx information services for aviation are still at the conceptual stage the current SWx providers will be a major source of SWx products for the aviation community. New SWx products can be tailored to better serve the operator needs in various scenarios and areas around the globe, based upon an already-established global standard. 492 12 493 2.2.1 Current Supporting Infrastructure from International Organizations 494 495 496 497 498 499 500 It is recommended that there be collaboration between ICAO, WMO, ISES, RWCs, and other meteorological authorities using their specific areas of expertise to develop an internationallyconsistent set of SWx products. To achieve this, it would be advantageous to form a small group of experts, perhaps from the existing IAVWOPSG ad hoc group working this ConOps, to mature these concepts into products (including a Space Weather Advisory); conduct ongoing verification; hone performance metrics; include collaborative decision-making processes, standards, and recommended practices; and develop additional guidance material. 501 2.2.1.1 502 503 504 505 506 ICAO defines the requirements for SWx warnings to aviation through relevant amendments to its Annex 3 – Meteorological Service for International Air Navigation. ICAO will provide oversight of new requirements and derivative products/services and procedures with the approval of the new Standard and Recommended Practice (SARP) for SWx Information for implementation in 2016. 507 2.2.1.2 World Meteorological Organization 508 509 510 511 512 The WMO is an integral part of the interoperability between the major stakeholders. The WMO Commission of Aeronautical Meteorology and the Commission for Basic Systems established the International Coordination Team for Space Weather (ICTSW) to support the IAVWOPSG efforts to integrate SWx services to terrestrial weather information delivery. The WMO will take ownership of and manage the requirements when tasked by ICAO once they are implemented. 513 2.2.1.3 International Space Environment Service 514 515 516 517 518 519 ISES is the primary international entity responsible for SWx services. Its mission is to encourage and facilitate near real-time global monitoring and prediction of the space environment, and to provide services to users that reduce the impact of SWx on activities of human interest to include aviation operations. The suite of SWx products and services are accessible to all domestic and international airline dispatchers and pilots, controllers, flight briefers, and planners, through 14 RWCs. 520 2.2.1.3.1 Regional Warning Centers 521 522 523 524 525 526 527 At present, there are 14 RWCs around the globe (Figure 4). The primary reason for the existence of the RWCs is to provide services to the scientific and user communities within their regions, as well as to provide guidance and training material. Perhaps a concept to establish regional centers for training should be considered. RWCs would be encouraged to provide SWx information in the form of observations, forecast, and climatology. Each RWC will tailor the SWx information it receives and integrate it into SWx products and services as warranted for its region of responsibility into standardized formats and content. 528 529 530 531 532 533 534 535 536 These services can consist of aviation-specific forecasts or warnings of disturbances to the solar terrestrial environment. The range of the locations of RWCs results in a very diverse set of users for these forecasts. An important feature of the ISES system is that each RWC is able to construct and direct its services to the specific needs of its own customers. There should be some consideration for expanding the providing service to include decision-makers involved concerning impacts on SWx communication and on the severity of impacts on GNSS subsystems in generic terms in time and region. This could include general information on the potential radiation that could affect avionics, passengers, and crews. Details of ISES and the RWCs can be found at http://www.ises-spaceweather.org/. 13 International Civil Aviation Organization 537 538 539 Each RWC must intra-connect its usual user community services within its own region, while working to harmonize and standardize product content, format, and procedural services, in order to promote seamless operational procedures for improved aviation efficiency. S. Korea 540 541 542 Figure 4: The RWC in Boulder has a Special Role in the “World Warning Agency,” Acting as a Hub for Data Exchange and Forecasts. 543 544 2.2.1.3.2 The NOAA Space Weather Prediction Center 545 546 547 The Space Weather Prediction Center (SWPC), in Boulder, Colorado, USA provides an end-toend process that collects and analyzes SWx observations to produce forecasts, warnings, and alerts for its customers—including airlines. 548 549 550 551 The SWPC plays a special role as the ISES “World Warning Agency,” acting as a hub for data exchange and forecasts.13 The data exchange is standardized in nature and format, ranging from simple forecasts or coded information, to more complicated content, such as imagery that the RWCs can utilize to provide services to the scientific and user communities within their regions. 552 553 The SWPC website provides a variety of SWx products that describe expected SWx conditions, including the following elements: 554 555 (a) SWPC provides real-time monitoring and forecasting of solar and geophysical events. 556 557 (b) SWPC provides near-real-time and recent data, solar and geomagnetic indices, and solar event reports. 558 559 560 SWx and meteorological services are two aspects of environmental information that are jointly needed in support of safety and sustainability of the airline industry. The SWPC website provides alert messages for SWx activities as follows: 13 NOAA, Space Weather Prediction Center (SWPC), Manual on Space Weather Effects in Regard to International Air Navigation, (January 2011). 14 561 Watch messages are issued for long lead times for all SWx activity predictions. 562 563 Warning messages are issued when some condition is expected. The messages contain a warning period and other information of interest. 564 565 Alert messages are issued when an event threshold is crossed and contain information that is available at the time of issue. 566 567 Summary messages are issued after the event ends, and contains additional information that was not available at the time of issue. 568 The following assumptions are made, relative to the SWx forecasts: 569 570 571 SWPC will continue to produce these alerts and forecasts. New SWx products in object-oriented graphical or gridded formats will be designed and proposed to ICAO for consideration and publication in Annex 3.14 572 2.2.1.3.3 Australian Space Weather Information Services 573 574 575 576 577 578 579 580 581 The Ionospheric Prediction Service (IPS), a service of the Australian Department of Industry, Science and Resources, has been producing air route HF prediction charts based on real-time and forecast ionospheric models for many years. The IPS is a specialist SWx unit of the Australian Bureau of Meteorology and provides a range of services to the Aviation Industry. These services include an auroral oval activity HF prediction product using Polar-Orbiting Environmental Satellites (POES) satellite data but could be augmented to use GOES data in Solar Energetic Particles (SEP) events. In addition, IPS has been producing Sudden Ionospheric Disturbance (SID)/Short-wave Fadeout Chart (SWF) charts based on GOES X-ray flux measurements for many years. Alerts are issued for HF fades based on solar X-ray flux. 582 583 584 585 586 587 588 589 590 In recent years, IPS has been working in consultation with the Australian aviation industry on the impacts of SWx on some sub-systems of the GNSS. The Australian research team is believed to be at the forefront in this area, and the team has investigated the impacts of SWx on Ground Based Augmentation Systems (GBAS) and the possibility of tolerance levels being exceeded during large geomagnetic storms. GBAS offers the ability to support multiple runway ends; reduced flight inspections and maintenance requirements compared to Instrument Landing System (ILS); a more stable signal; and less interference with preceding aircraft. GBAS/WAAS is a safety-critical system that augments the GPS Standard Positioning Service (SPS) and provides enhanced levels of service. 591 592 593 594 595 Polar Cap Absorption (PCA) events are typically monitored using high-energy proton data from the GOES satellites. IPS also monitors PCA events using a ground-based array of Relative Ionospheric Opacity Meters (riometers – see Appendix B), which can be used as an alternative to satellite data. For an industry such as aviation, perhaps ground-based alternatives should also be considered to satellite data wherever available. 596 597 IPS has been working with Qantas Airlines on improving the Australian aviation industry understanding of radiation hazards from SWx. 598 3 599 600 Unlike other known weather hazards that are usually linked to specific FIRs, SWx is typically a global-scale phenomenon. Despite the evolving constellation of SWx monitoring satellites, space DESCRIPTION OF CHANGES 14 Space Weather Sub-Group of the Cross Polar Working Group, “Integrating Space Weather Observations & Forecasts into Aviation Operations, Aviation Space Weather User Requirements,” Version 3.02, (November 2010). 15 601 602 603 604 and ionospheric observational data is sparse and the current models are unable to predict with reasonable confidence, the pertinent eruptive activity that will significantly impact the Earth’s magnetosphere. The forecast depicts the intensity of the solar event and other important aspects involving the time of onset and expected duration of this SWx hazard. 605 606 607 608 609 An additional change that has been requested by some aviation users pertains to the characterization of solar radiation events. The SWx science and aviation community is encouraged to collaborate on developing and providing an appropriate SWx scale that would be based upon the relevant part of the corresponding energy spectrum of the impinging protons, and be assessed with appropriate reliable space-borne measuring instruments. 610 611 612 613 SWx forecast products, although produced back to the Apollo missions in the 1960s, are in a formative phase for the purposes of aviation. The initial lists of objectives below will be targeted to meet accuracy and dependability requirements as prescribed in more detail in Appendix D. But this list is by no means exhaustive. Objectives include: 614 615 616 617 Continued provision of real-time solar wind data for the models and their output to forecasters from the replacement spacecraft for the ACE, NASA’s Deep Space Climate Observatory (DSCOVR) spacecraft vehicle, along with other space-based observing platforms to foster better numerical model output and forecaster input 618 619 620 Refinement of probabilities both from a user and a ATM standpoint as presented in Table 5. Improved forecast accuracy and reliability as heliospheric space physics models evolve 621 622 Improved forecast to accurately identify and predict the time, duration, and intensity of SWx events for aviation users as defined in the functional requirements in Appendix C 623 Ability to forecast solar eruptive activity prior to initial event 624 Improved identification of affected area from impacts (i.e., HF outage) 625 Probability output disseminated in gridded format 626 627 628 Standard SWx forecasts by all advisory centers with respective procedures that precipitate from such information coming from various sources, for example, something similar to the NOAA Space Weather Scale 629 630 631 632 633 634 635 636 The communication gap between providers of SWx information and the airline industry will need to be streamlined. SWx advisories are often Nowcast-type forecasts that err on the side of caution, issuing potential solar storm-scale intensity indices greater than what actually transpires. This typically shifts flight maneuvers to lower altitudes, reducing potential radiation exposure— but adding time and duration to the flight path, and in the worst cases, leads to costly en route diversions and delays. Insufficient detection and unnecessarily coarse modeling of SWx are two of the major shortfalls toward developing reliable forecasts of the SWx hazards for the specific duration and intensity thresholds affecting communications, navigation, and radiation exposure. 637 638 639 640 641 642 Prior to the implementation of this initial set of requirements, it would be advantageous to hold another Space Weather Workshop (similar to AMS policy conference held in Washington, DC, November 2006) for core end users specifically addressing the uncertainties confronting meteorological product format and service delivery, and including clarification of communication links, the roles and responsibilities of various organizations within the international echelon structure, and regional training and education. 16 643 644 3.1 Proposed Service Description 645 3.1.1 646 647 648 649 650 651 The need for new and improved SWx information becomes more apparent with the continued growth in polar air routes, near-term commercial spaceflight (suborbital space tourism), and advances in nano-technology (microelectronics). Before SWx data are provided to the users, it must be determined what type of data is needed, what thresholds are needed, and when the data should be disseminated. Similarly, SWx information and service providers need guidance on standardizing the information for the aviation industry. 652 653 654 655 656 657 658 659 660 SWx information needs to be standardized by classification type and sourced in a manner that parallels methods used for terrestrial weather, and is familiar to the users of SWx. For example, the NOAA Space Weather Scales (Table 1, Table 2, and Table 3) currently provide standardized formats of impacts classified by storm type and intensity. The scales list the intensity and frequency of occurrence for radio blackouts, solar radiation storms, and geomagnetic storms. SWPC uses these scales to categorize the severity of impact.15 Development and delivery of SWx information and services in this format should be considered for acceptance as the global standard to ensure the data will be available on a global scale and that the display of data will be similar to what is already in place. 661 662 663 664 665 666 Either the NOAA Space Weather Scale or another internationally-approved standard of index thresholds must be adopted and uniformly used in the forecast on the flight deck and in Traffic Flow Management (TFM) DSTs. Whatever the approved Space Weather Scales end up being, they should be incorporated into flight planning tools for characterizing duration, the type of SWx hazard and its severity. The SWx information and format should be a single global standard for aviation operations. 667 668 669 The current threshold values or indices related to particular SWx parameters are shown below. Note that some of these threshold values might be improved and better tailored for current operational needs.16 670 671 672 673 674 675 In recent Solar Cycles (1976-2008), the rate of occurrence of Solar Radiation Storms has increased over those referenced in the NOAA Space Weather Scales. The recent cycles reveal average updated numbers as follows: S1 Minor = ~ 75 per cycle, S2 Moderate = ~33 per cycle, and S3 Strong = ~12 per cycle. After some comprehensive analysis for geomagnetic storms, the number of days per cycle for G-scale events shows: G1-950 days/cycle, G2=390 days/cycle, G3=140 days/cycle, G4=50 days/cycle, and G5 = 3 days/cycle. 676 The current threshold values or indices related to particular SWx parameters are shown below:17 677 678 679 Radio Blackouts: Fluxes in X-ray and Extreme Ultra Violet (EUV) photons burst from solar flare arriving in eight minutes (speed of light) measured in the 0.1-0.8nm range. But other physical measures are also considered. 680 681 682 Solar Radiation Storms: The index for high energy proton particle fluxes are five minute averaged measurements derived from energies >10MeV proton flux. However, protons >100MeV are better indicators of radiation to passengers and crew but the expansion through the Standardizing Aviation Space Weather Information 15 SWPC website: www.swpc.noaa.gov (NOAAScales). SWPC website: www.swpc.noaa.gov (Alert/Warnings). 17 SWPC website: www.swpc.noaa.gov (Alert/Warnings). 16 17 683 684 development of an S-scale may become more apparent as expertise is gained with NAIRAS and the event driven radiation dose level. 685 686 687 Geomagnetic Storms: The K-index is used to determine this SWx element and its intensity is displayed as K-1 – K9, with 9 being the most intense. Currently, messages are automatically generated from real-time measurements of a distributed magnetometer network. 688 689 690 See Appendix E for more details on specific thresholds that trigger the various SWx alert messages that are in concert with the NOAA Space Weather Scales presented in Table 1, Table 2, and Table 3 below. 691 692 693 See Appendix H for more details on the effort for SWx information to be globally standardized for geomagnetic field intensity and expected impacts in a temporal and spatial sense. 694 18 695 Table 1: NOAA Space Weather Scale for Radio Blackout Events Radio Blackouts HF Radio: Complete HF (high frequency**) radio blackout on the entire sunlit side of the Earth lasting for a number of hours. This results in no HF radio contact with mariners and en route aviators in this sector. R5 Extreme Strong 696 697 698 699 (2x10-3) X10 8 per cycle (10-3) (8 days per cycle) X1 175 per cycle (10-4) (140 days per cycle) M5 350 per cycle (5x10-5) (300 days per cycle) M1 2000 per cycle Navigation: Low-frequency navigation signals degraded for about an hour. Moderate Navigation: Degradation of low-frequency navigation signals for tens of minutes. HF Radio: Weak or minor degradation of HF radio communication on sunlit side, occasional loss of radio contact. R1 Fewer than 1 per cycle Navigation: Outages of low-frequency navigation signals cause increased error in positioning for one to two hours. Minor disruptions of satellite navigation possible on the sunlit side of Earth. HF Radio: Limited blackout of HF radio communication on sunlit side, loss of radio contact for tens of minutes. R2 X20 Severe HF Radio: Wide area blackout of HF radio communication, loss of radio contact for about an hour on sunlit side of Earth. R3 Number of events when flux level was met; (number of storm days) Navigation: Low-frequency navigation signals used by maritime and general aviation systems experience outages on the sunlit side of the Earth for many hours, causing loss in positioning. Increased satellite navigation errors in positioning for several hours on the sunlit side of Earth, which may spread into the night side. HF Radio: HF radio communication blackout on most of the sunlit side of Earth for one to two hours. HF radio contact lost during this time. R4 GOES X-ray peak brightness by class and by flux* Minor Navigation: Low-frequency navigation signals degraded for brief intervals. (10-5) (950 days per cycle) * Flux, measured in the 0.1-0.8 nm range, in W·m-2. Based on this measure, but other physical measures are also considered. ** Other frequencies may also be affected by these conditions. 19 700 Table 2: NOAA Space Weather Storm Scale for Radiation Storm Events Solar Radiation Storms Biological: unavoidable high radiation hazard to astronauts on EVA (extra-vehicular activity); passengers and crew in high-flying aircraft at high latitudes may be exposed to radiation risk. *** S5 Extreme Flux level of > 10 MeV particles (ions)* Number of events when flux level was met** 105 Fewer than 1 per cycle 104 3 per cycle 103 10 per cycle 102 25 per cycle 10 50 per cycle Satellite operations: satellites may be rendered useless, memory impacts can cause loss of control, may cause serious noise in image data, startrackers may be unable to locate sources; permanent damage to solar panels possible. Other systems: complete blackout of HF (high frequency) communications possible through the polar regions, and position errors make navigation operations extremely difficult. Biological: unavoidable radiation hazard to astronauts on EVA; passengers and crew in high-flying aircraft at high latitudes may be exposed to radiation risk.*** S4 Severe Satellite operations: may experience memory device problems and noise on imaging systems; star-tracker problems may cause orientation problems, and solar panel efficiency can be degraded. Other systems: blackout of HF radio communications through the polar regions and increased navigation errors over several days are likely. Biological: radiation hazard avoidance recommended for astronauts on EVA; passengers and crew in high-flying aircraft at high latitudes may be exposed to radiation risk.*** S3 Strong Satellite operations: single-event upsets, noise in imaging systems, and slight reduction of efficiency in solar panel are likely. Other systems: degraded HF radio propagation through the polar regions and navigation position errors likely. Biological: passengers and crew in high-flying aircraft at high latitudes may be exposed to elevated radiation risk.*** S2 Moderate Satellite operations: infrequent single-event upsets possible. Other systems: effects on HF propagation through the polar regions, and navigation at polar cap locations possibly affected. Biological: none. S1 Minor Satellite operations: none. Other systems: minor impacts on HF radio in the polar regions. 701 702 703 704 705 * Flux levels are 5-minute averages. Flux in particles·s-1·ster-1·cm-2. Based on this measure, but other physical measures are also considered. ** These events can last more than one day. *** High energy particle measurements (>100 MeV) are a better indicator of radiation risk to passenger and crews. Pregnant women are particularly susceptible. 706 707 20 708 Table 3: NOAA Space Weather Storm Scale for Geomagnetic Storm Events Geomagnetic Storms G5 Extreme Power systems: widespread voltage control problems and protective system problems can occur, some grid systems may experience complete collapse or blackouts. Transformers may experience damage. Kp values* determined every 3 hours Number of storm events when Kp level was met; (number of storm days) Kp=9 4 per cycle (4 days per cycle) Spacecraft operations: may experience extensive surface charging, problems with orientation, uplink/downlink and tracking satellites. Other systems: pipeline currents can reach hundreds of amps, HF (high frequency) radio propagation may be impossible in many areas for one to two days, satellite navigation may be degraded for days, lowfrequency radio navigation can be out for hours, and aurora has been seen as low as Florida and southern Texas (typically 40° geomagnetic lat.).** Power systems: possible widespread voltage control problems and some protective systems will mistakenly trip out key assets from the grid. G4 Severe Kp=8, including a 9- 100 per cycle Kp=7 200 per cycle Spacecraft operations: may experience surface charging and tracking problems, corrections may be needed for orientation problems. (60 days per cycle) Other systems: induced pipeline currents affect preventive measures, HF radio propagation sporadic, satellite navigation degraded for hours, lowfrequency radio navigation disrupted, and aurora has been seen as low as Alabama and northern California (typically 45° geomagnetic lat.).** Power systems: voltage corrections may be required, false alarms triggered on some protection devices. G3 Strong (130 days per cycle) Spacecraft operations: surface charging may occur on satellite components, drag may increase on low-Earth-orbit satellites, and corrections may be needed for orientation problems. Other systems: intermittent satellite navigation and low-frequency radio navigation problems may occur, HF radio may be intermittent, and aurora has been seen as low as Illinois and Oregon (typically 50° geomagnetic lat.).** Power systems: high-latitude power systems may experience voltage alarms, long-duration storms may cause transformer damage. G2 Moderate Kp=6 600 per cycle (360 days per cycle) Spacecraft operations: corrective actions to orientation may be required by ground control; possible changes in drag affect orbit predictions. Other systems: HF radio propagation can fade at higher latitudes, and aurora has been seen as low as New York and Idaho (typically 55° geomagnetic lat.).** Power systems: weak power grid fluctuations can occur. Spacecraft operations: minor impact on satellite operations possible. G1 709 710 711 712 713 Minor Kp=5 1700 per cycle (900 days per cycle) Other systems: migratory animals are affected at this and higher levels; aurora is commonly visible at high latitudes (northern Michigan and Maine).** * The K-index used to generate these messages is derived in real-time from the Boulder NOAA Magnetometer. The Boulder K-index, in most cases, approximates the Planetary Kp-index referenced in the NOAA Space Weather Scales. The Planetary Kp-index is not yet available in real-time. ** For specific locations around the globe, use geomagnetic latitude to determine likely sightings 21 714 3.1.2 Integration and Delivery of Space Weather Meteorological Services 715 716 717 718 719 720 721 722 723 Sensing, understanding, forecasting, and applying information relating to conditions in the nearEarth space environment are key components of monitoring SWx. In order to provide accurate and reliable warnings for pending hazardous solar activity events, observations of electromagnetic energy and energetic particles are crucial.18 SWx forecast attempt to predict conditions that occur near the Earth, when the Sun erupts with enhanced photons, high energy charged particles and magnetic field. It is recommended a conceptual simplified SWx information user display or text product should be developed, perhaps in some gridded data format integrating the potential intensities referenced from the NOAA Space Weather Scales in polygons considering the latitude, time of day, etc. 724 725 726 727 728 729 While the NOAA Space Weather Scales are very useful for generalizing SWx events and providing some indication of latitudinal dependence, the effects of the associated SWx events at various latitudes can vary quite significantly on various technologies such as the GBAS/WAAS, power networks, aircraft radiation levels, short-waves fadeout, HF communication frequencies, etc. 18 OFCM/OSTP, Impacts of NPOESS Nunn-McCurdy Certification and Potential Loss of ACE Spacecraft Solar Wind Data on National Space Environmental Monitoring Capabilities (January 2008). 22 730 4 PROPOSED CONCEPT 731 4.1 732 4.1.1 Assumptions for Airline Industry Operations 733 734 735 736 737 The economic impact of SWx is significant and continues to grow. The airline industry’s vulnerability increases with the growing number of daily trans-polar commercial flights and their reliance on satellite technologies and communication frequencies vulnerable to effects of SWx. GNSS allows every country to develop positioning, location, and timing services for its own constituency. The largest potential for failure or degraded service is imposed by SWx. 738 4.1.2 Constraints to Providing Robust Space Weather Products and Services 739 740 741 742 743 744 745 746 747 748 749 750 751 There are recommendations to ensure the SWx products and service formats are universally accepted and efficiently disseminated in a time-sensitive manner to be relevant for user needs: 752 753 754 755 756 757 A common theme would help focus and maintain the international community effort toward global harmonization of SWx information in a single standard. Global aviation operations generally execute using some sort of a daily (or cyclic) schedule of collaborative decisionmaking that reaches consensus in mapping out a sensible, cost-effective air traffic strategy. The science and human-in-the-loop elements utilize a multitude of communicative and tracking systems to create and disseminate standard and/or tailored SWx information products. 758 759 760 761 762 763 764 765 766 767 768 769 770 771 772 A virtual exercise, which is a low-cost and effective method to evaluate how this process could evolve into a single global standard for products and services, should be conducted. This virtual exercise could serve to validate the requirements (Appendix C) and would articulate the causes of SWx impacts along the polar airline routes open to commercial traffic. This exercise could utilize ongoing operations and conduct virtual simulations in a non-intrusive manner to evaluate real-world situations of all the potentially hazardous effects, without the real-world consequences. Analysis and its derivative impact assessment can be conducted in a less stressful environment. The assessment would focus on safety, time, and operating cost aspects over longhaul flights as a result of en route modifications or flight plan changes from observed or forecasted incoming highly charged energy particles (solar storms) traveling along the Earth’s magnetic field lines downward through aviation altitudes toward the magnetic—not geographical—pole. These ionized particles cross through the normal aviation altitudes en route across the polar region, impacting navigation, communications, and radiation exposure to crew and passengers. The concept of conducting such an exercise was driven by documented operator needs for aviation SWx. Assumptions and Constraints 1. ICAO does not currently provide standards and recommended practices for the provision of SWx information in Annex 3 or provide specific guidance in any other manual or publication. 2. To support Global ATM, SWx information must be accessible and usable by a variety of aviation decision-makers, including flight crew members. 3. Bandwidth limitations, particularly on oceanic and polar routes, may limit the types of SWx information that can be efficiently transmitted to the aircraft to support en route decisions by flight crew members. 4.2 Operational Environment 23 773 774 775 776 777 778 Meeting the criteria of the confidence levels in Table 5 provides the ability for operators and air traffic services to mitigate the impact of adverse SWx along long-haul polar routes shown in Figure 1. Improving the monitoring and sensing of the spatial and temporal elements of SWx will improve the reliability and confidence levels of SWx forecast products. These would help mitigate communication and avionics’ equipment degradations, and human health threats, while increasing the socio-economic benefit, efficiency, and safety for the aviation industry. 779 780 781 782 783 784 785 786 The Australian Department of Industry, Science and Resources IPS is developing an extreme SWx service that will be based on a count-down style warning system from the initiation of the event on the Sun, through the solar wind to Earth and the subsequent impact on national infrastructures. The count-down scale runs from a Level 5 (initialization of event) to a Level 0 (storm in progress or significant impact on a particular technology based on relevant thresholds). Perhaps this count-down method should be considered as an alternative or modified, worthy of further investigation, to the current “watch,” “warning,” and “alert” levels and message format utilized in some portions of the globe. 787 788 789 790 791 792 793 794 The proposed set of SWx requirements (Appendix C) considers a modified message format, time frequency issued, and intervals updates. An example is a theoretical scenario warranting the need to amend the 30-hour forecast cycle product (shown in Table 5 and Appendix C) during some demonstration period. This exercise would help assess whether the frequency and type of product is adequate in serving all phases of aviation operations effectively and reliably. Additionally, conducting regional exercises might be a way to evaluate the send and receive mode of SWx information from the global centers and meteorological facilities and to ensure effectiveness and speed of response, in a manner similar to IAVWOPSG warnings from volcanic eruptions. 795 Table 4: User Needs to Better Understand and Mitigate SWx Impacts on Aviation Operations Needs for Global Harmonization of SWx Information in a Single Standard for Aviation 1 2 3 4 796 797 798 Improved detection of solar, interplanetary, ionospheric and atmospheric variables related to SWx Improved forecasting SWx models Improved current and forecast SWx products Better dissemination of the products to users Understanding how terrestrial weather is standardized for aviation will help SWx and ANSP configure information and services for efficient delivery. The capabilities to do this are presented as follows: 799 800 801 a) Remote Sensing: Evolving Heliophysics System Observatory–Spacecraft Constellation looking at the Sun in total in four-dimensions (e.g., STEREO, Two Wide-Angle Imaging Neutral-Atom Spectrometers [TWINS-2], etc.) 802 803 804 805 806 807 808 809 b) In Situ Observations: A multitude of space-based satellites are monitoring and sensing SWx phenomena. But the only SWx station to provide ground truth similar to a groundbased Automated Surface Observing System (ASOS) station on Earth for terrestrial weather is the ACE spacecraft. The ACE directly measures charged protons and electrons traveling on the associated solar wind at speeds in the millions of miles per hour, and from various types of solar events. This is an aging research satellite, well beyond its life expectancy. Its replacement is the DSCOVR spacecraft, projected to be launched in 2014. A fleet of other deep space satellites including SOHO, STEREO, SDO and other 24 810 811 observational spacecraft platforms are monitoring on a continuous basis the properties of solar wind, the interplanetary magnetic field, and SEP. 812 813 814 815 816 817 818 c) Nowcasts/Forecasts: The result of a multitude of complex SWx models coming-of-age over the last decade. Two examples of SWx models supporting aviation operations are the D-Region Absorption Product (D-RAP) and the Wang-Sheeley-Arge (WSA) Enlil (named for the Sumerian god of wind). These models are defined further in section 4.3.1 under #5. Another example for future widespread availability is the advanced space physics- and/or empirical-based models (e.g., Global Assimilation of Ionospheric Measurements [GAIM], etc.). 819 820 821 822 Figure 5 shows how SWx information providers who produce forecasts, analyses, and other SWx products will receive and disseminate pertinent and reliable streamlined services in near real time that will help improve all phases of flight planning and execution. This should include, but is not limited to: 823 Currency of the product (product issue and valid times) 824 Relevance of the product 825 Cause of the hazard 25 M a nu r e c t i ves / / Pilot Pilot Aircraft Aircraft Research Observations Community Space Weather iD d o Pr u c 2002 2001 10993 i gn o to r S W PC Data for model improvement /I nt e s a l n o E S i S Crosslink ofevent avionic information equipment between malfunction aircraft M 827 826 Figure 5: Future Production and Communications Concept 828 829 830 831 832 833 834 835 In addition, the new concept of a cross-link between en route aircraft for passing real-time avionic equipment malfunctions (single and multiple-bit upset information shown at the top of figure) should be considered. It is recommended that some type of possible pilot actions should be listed at the ready within the cockpit, when expected conditions warrant such information to be provided rather than pilots performing their own freelance SWPC monitoring in the form of an alerting service. One such option this could be done would be through an Aircraft Communications Addressing and Reporting System (ACARS) accessible to high-level Significant Meteorological (SIGMET)-like forecast information.19 But this option is not the most 19 ICAO Annex 3, World Area International Air Navigation, Chapter 3, Meteorological Watch Offices, Appendix 2, WAFS, 17th Edition (July 2010). 26 Traffic Density of Polar Routes a Downl i nk t Flow of Space Weather Information a d 836 837 838 839 desirable, as some solar events have a rapid onset of high radiation levels. Timeliness of the information is critical, and off-time ACARS requests do not seem to guarantee the required, short information-transmission line. 4.3 Operations 840 4.3.1 Existing and Future Space Weather Information 841 842 843 844 845 A required component of all flight operations is the pre-flight weather briefing. Prior to every flight, pilots and airline dispatchers must gather all information vital to the flight. Meteorological information is necessary to ensure a safe and efficient flight. This should include appropriate SWx information applicable for the operation, and that is obtained from recognized official reference sources (see Table 8Table 8). 846 847 848 The SWx information for use by airline pilots and dispatchers while planning and dispatching a flight should provide as complete a SWx picture as possible, focusing on any anticipated impacts on communications, navigation, and radiation exposure risk. 849 850 Examples of the types of existing and future SWx information to include in a standard briefing prior to the departure of any flight include the following: 851 852 853 854 855 1. Adverse Conditions: Conditions resulting from a SWx event, including adverse conditions that may influence a decision to cancel or alter the flight route. Adverse conditions include significant SWx, such as loss or disruption of communications, increased levels of radiation at planned altitudes, and NOAA Space Weather Scales intensities related to GNSS affecting navigation. 856 857 858 859 2. Synopsis: The synopsis along or near the intended route of flight should be an overview of the weather picture including SWx and any resulting impact effects from the solar activity (i.e., flares, geomagnetic storms and its associated activity, ionospheric variations, and aurora borealis/australis). 860 861 862 3. Current Conditions: Current SWx observations affecting communications, radiation, and navigation along the route of flight. Nil activity, effects, and degradation should be stated. 863 864 4. En Route Forecast: A summary of the SWx forecast affecting communications, radiation, and navigation for the proposed route of flight. 865 866 867 868 869 870 871 872 873 874 875 876 5. Communication Frequency Forecast: Where applicable, detailed information on the best (max) useable HF frequencies, within a time period, in each ATC FIR. An example of a forecast output is the D-Region Absorption Product (D-RAP) provided to airlines and dispatchers with a map indicating where HF communications are compromised by SWx phenomena. D-RAP is driven by GOES X-Ray data, energetic particle data, and ground magnetometer data, and is undergoing verification through cooperation of Canada’s Space Weather Forecast Centre. It is constructing a network of HF transmitters/receivers to mimic airline communication in real time against the pilot reports logging radio frequency and contacts, and broken contacts. The WSA Enlil model provides the latest forecast of conditions in the solar wind, improving NOAA’s forecast skill. The solar wind is a fast moving stream of charged particles emanating from the sun and moving outward towards the Earth and planets. 877 878 879 6. Integrity Reduction of GNSS and Satcom: A provision to monitor associated level of services to warn of reduction with GNSS and satellite communications in real time. Discussions are ongoing to make this a requirement of airlines after further consideration. 27 880 881 7. Radiation Aloft: A forecast of the atmospheric radiation dose rates expected to be encountered at specific altitudes and latitudes along the route of flight. 882 883 8. ATC Delays: An advisory of any known or anticipated ATC delays or spacing variations, due to SWx activity, that may affect the flight. 884 885 9. Other Information: Contact information, or the telephone number of the National ISES RWC. Any additional information requested should also be provided in this section. 886 4.3.2 Future Targets for Outlook Information 887 888 889 890 891 892 893 894 895 896 The reliability and confidence levels or probability (%) of a forecast event is crucial, not only for increasing operational efficiency and safety, but also for mitigating unnecessary costs. SWx events can affect large volumes of airspace over long timescales, leading to large commercial impacts. Therefore, it is imperative that operational decision-makers have better confidence in the accuracy of observations obtained and the SWx Probability of Detection (POD) forecasts. Each SWx product the percentage confidence level will vary depending on the POD. Table 5 provides the breakdown by product type of the confidence levels at different forecast timeframes expected for the future. However, the percentage confidence levels will vary depending on the Probability of Detection. 28 897 Forecast 7 days 7days 3 days 3 days 30-hrs 30-hrs 2025 2016 2025 2016 2025 2016 65-85% 35-55% 65-85% 45-65% 75-95% 55-75% Warning Alert 0 hrs Dispatcher Issued as Warranted Audio-visual 2016: 6-hr 75% “Attentiongetter” icons 2025: 6-hr 95% Parameter Changes 2016: 6-hr 75% 2025: 6-hr 95% Update Parameter Changes 2016: 6-hr 75% 2025: 6-hr 95% Post-Event Analysis 898 99% As Required by End User Table 5: Summary of General (%) Confidence Levels in Future Forecast Products 899 900 29 901 4.4 902 903 904 905 Improving the integration of SWx with terrestrial weather information now falls under the established purview of ICAO with assistance from the WMO as part of its charter. This integration is expected to improve efficiency and safety of air traffic management through established procedures and communication tools.20 906 907 908 909 910 911 This ConOps identifies and summarizes the high-level operational requirements and the supporting incremental, more detailed functional requirements. These requirements were gleaned from the “Aviation Space Weather User Service Needs” document developed by the CPWG Space Weather (SWx) Sub-Group. The 20 Aviation User Needs (AUN) statements were defined and reached by consensus with participating member air navigation service providers in December 2010. 912 913 914 A functional analysis was performed on these AUNs, incorporating critical content from the document, and allowing for responsible, accountable requirements to be written. The definition of these operational and functional requirements has been defined in Appendix C. 915 916 917 918 919 The initial set of AUNs (Table 6) are the back-drop of an associated set of operational and unallocated functional requirements drafted in Appendix C, and proposed for international acceptance. These requirements were developed from the following 20 AUN-defined consensus statements from the CPWG SWx Sub-Group: 20 Operational Requirements WMO Space Programme SP-5, “The Potential Role of WMO in Space Weather” (April 2008). 30 Derived Statement of Need for Space Weather AUN-1 Define the impacts of space weather AUN-2 Provide the following types of information: observations, forecasts, and climatology AUN-3 Provide information in text and graphical format AUN-4 Present information using standardized format and content AUN-5 Describe/display the severity of impact in standardized text and graphical reports AUN-6 Provide text and graphical reports using specified timelines and durations AUN-7 Provide an estimate of the accuracy of the information AUN-8 State the regions affected AUN-9 Utilize stated transmission methods for space weather reports AUN-10 Provide information on disruptions to HF communications AUN-11 Provide information on disruptions to VHF communications AUN-12 Provide information on disruptions to UHF communications AUN-13 Provide information on fading and loss of lock to SATCOM AUN-14 Provide information on the radiation environment that will affect avionics AUN-15 Provide information on the radiation environment that will affect humans AUN-16 Provide Information that will affect GNSS AUN-17 Define space weather information and decision-maker matrices not included AUN-18 Define communication and integration of space weather information not included AUN-19 Provide space weather education and training not included AUN-20 Use global standards for space weather information not included 920 Table 6: Aviation User Need Statements 921 922 923 924 925 When the operators reach a consensus on what service needs are warranted, a functional analysis will be performed. A functional analysis translates operators’ needs and human performances (capabilities and limitations) into a sequence of top-level functions deconstructed to lower-level building block-type functions. These collective functions define and depict the needed service or operational capability that will become the primary foundation for framing requirements. 926 927 4.5 928 929 930 SWx information needs to be integrated with the flight planning process and disseminated for the end user alongside terrestrial weather for the end users, in a manner similar to terrestrial weather, and presented in an understandable format actionable for even the novice aviation industry user. Supporting Infrastructure 31 931 932 933 The method of delivery of SWx products and reports should be seamless and conform to existing protocol so it can be ingested by DSTs and easily displayed and understood at the lowest common denominator. 934 935 In addition, SWx products and services should be made available to maintenance and engineering personnel for post-event analysis in the event of avionic upsets or GNSS outages. 936 937 SWx information can be either “pushed” or “pulled,” and if required, integrated with the operations/dispatcher work area as follows: 938 939 940 941 942 943 Pushed: Authorized service provider delivers international meteorological terminology products that may or may not parallel the content format described earlier in this document for the SWPC Warnings, Alerts, Updates, Text, and Alert graphics. But the SWPC graphics themselves do not use the normal international meteorological vocabulary. Terminology usage and format will have to be determined. The current rules are prescribed within ICAO Annex 11 governing the Alert Service. 944 945 946 Pulled: “Flagged Icons” (format and terminology, TBD) to immediately notify operators/dispatchers of Warnings, Alerts, Updates, Text product messages and/or Alert graphics. 947 948 949 Focus should be on significantly increasing the safety, security, and capacity of air transportation operations. The key capabilities will rely on network-enabled information sharing that will ensure information is available, secure, and usable in real time across air transportation domains. 950 951 952 SWx information is needed to support operational decisions for the polar routes by airline operations centers, flight crews, and ANSPs. Table 7 identifies the various users and the information needed for decision making. 953 954 955 956 957 Table 7 is based upon similar decision areas and criteria taken from the latest draft document for the Preliminary Performance Requirements (Version 0.2c, September 10, 2008).21 The additional “Xs” (in red) indicate recommendations the operators see as necessary for them to operate in a responsible and safe manner. These additional “Xs” are not operational requirements at this juncture, but critical user needs considered for adoption and implementation down the road. 958 The tables cross-reference the SWx information with the decision-makers. 959 960 Note: Black “Xs” indicates the user requires this information for decisions. These users include the following: 21 JPDO Weather Functional Requirements Study Group, “Four-Dimensional Wx Functional Requirements for NextGen Air Traffic Management, Version 0.2” (February 15, 2008). 32 x x x x X x X X x x X x x x x x X X X x X x x x x x x x x x x x x x x x x X X x x x x x X x x x x x x x x x x x x x x Metering/Spacing Decision x Local Controllers Arrival/Departure Route Selection x x Route/Altitude Selection x x Approach/Departure Controllers Metering/Spacing Decision X x Approach/Departure Clearance X x Approach/Departure Route Selection X Route/Altitude Selection X Landing Decision x Metering/Spacing Decision Approach Commencement x Hazardous Weather Deviation x In-flight Route/Altitude Change x Route/Altitude Selection x x Go/No Go Decision x Oceanic Controllers En Route Controllers Metering/Spacing Decision Airport/Spaceport SW Reports Airport/Spaceport Terminal SW Forecasts En Route SW Forecasts SW Alerts and Warnings x Pilots Route/Altitude Selection Disruption/loss of HF Comms Interruption of VHF Comms Reduced UHF Performance Interruption of SatCom Radiation Environmental levels and variability GNSS integrity, accuracy and outages In-flight Route/Altitude Change Information Types Go/No Go Decision Decisions Airline Dispatchers or Support Route/Altitude Selection Decision-makers x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x 961 Airport/Spaceport SW Reports Airport/Spaceport Terminal SW Forecasts En Route SW Forecasts SW Alerts and Warnings 962 x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x x X x x x x x x x x x x x x x x x x x x x x x x x x Spaceport, Runway Utilization x x x x x x x x x x x x x x x x x x x x x x x x x x x x Table 7: SWx Information versus Decision-maker Matrices 33 x Launch Operator or Pilot In-Flight Trajectory Change x Abort Decision x Go/No-Go Launch Decision x Departure Location/Trajectory Decision Metering/Spacing Decision x SWAP Implementation x Route Change x Ground-Stop/Delay Decision x Airport Acceptance Rate Determination Metering/Spacing Decision x SWAP Implementation x Aerospace Operators/ Controllers (Space Operations Centers) Air Route Traffic Managers Route Change x Ground-Stop/Delay Decision x Airport Acceptance Rate Determination Metering/Spacing Decision x SWAP Implementation Disruption/loss of HF Comms Interruption of VHF Comms Reduced UHF Performance Interruption of SatCom Radiation Environmental levels and variability GNSS integrity, accuracy and outages Route Change Information Types Ground-Stop/Delay Decision Decisions Approach/Departure Traffic Managers Traffic Managers Airport Acceptance Rate Determination Decision-makers x x x x x 963 4.6 Science Benefits to Be Realized 964 965 966 967 968 969 1. Improved SWx monitoring platforms and their respective measuring capabilities of space phenomena will result in a greater number of observations, better quality of such, and thereby, improved forecasts. The SWx information responsible for this will be harmonized, which implies its interpretation be uniform and the procedures be carried through in a seamless manner (single standard) that would mitigate operational cost to the airlines. 970 971 972 2. This establishment of methodologies from reference document sources, existing infrastructure, and products to help align the presentation of SWx information to include standardized information, format, and impacts (e.g., NOAA Space Weather Scales). 973 974 975 976 977 978 979 3. Some company policies discourage using current NOAA Space Weather Solar Radiation Storm Scales to provide information of radiation exposure to passengers and crews, since the information is based upon the integral flux of protons with energies above 10 MeV (proven inappropriate as an outcome from the 2012 Space Weather Aviation Workshop). Measurements > 100MeV are needed, and > 300Mev preferred as more appropriate. Future observation capabilities will eventually be able to provide those measurements on a routine basis. 980 981 4.7 Cost Benefits Associated with Polar Routes 982 983 984 985 986 987 1. During times of disturbed SWx activity, polar airline routes are often diverted to lower latitudes in order to prevent loss of radio communications and avoid human exposure in case of increased radiation from SEPs. Such flight diversions can cost airlines as much as $100,000 per flight for additional fuel, extra flight crew, and additional landing fees.22 This does not include indirect expenses or unquantifiable losses to passengers, like missed connections. 988 2. Benefits expected from the addition of SWx capabilities include: 989 990 991 a. More accurate and timely information for flight planning and determination of SWx impacts, including degraded or lost communications, erroneous navigation readings, and radiation exposure to flight crews and passengers. 992 993 994 b. Improved flight route optimization by flight dispatchers and pilots through more accurate and higher confidence forecast outputs with lead times required to meet industry needs. c. 995 996 997 998 999 1000 22 Diversions to mid-latitudinal routes that avoid the polar cap absorption effects on airline communications with ATM cost additional time, require more fuel, and reduce passengers and cargo carried per flight. Aircraft cost hundreds of dollars per minute to operate, so saving just minutes over a long-haul flight can save significant operating resources. As an example, a flight leaving Vancouver for Delhi takes 18 hours by traditional air traffic routes, but only 13.5 hours over the polar cap with fuel WMO Space Programme SP-5, The Potential Role of WMO in Space Weather (April 2008). 34 1001 1002 savings in the hundreds of thousands of dollars per flight. Flights from New York to Hong Kong save nearly five hours.23 1003 5 1004 1005 1006 1007 This ConOps document and the following functional and performance requirements are intended to be solution-independent. 1008 1009 1010 1011 The functional requirements are incremental tasks, or the building blocks necessary, to meet the higher level operational requirements. These requirements identify what must be done to meet the operator service needs, and format, and contents and are based upon the Space Weather Functional Analysis performed on those needs. 1012 1013 1014 1015 1016 1017 1018 This ConOps provides a common vision of what operator needs are required for a SWx system of support services to function from an operational perspective in the timeframe of 2016 and beyond. A description of what is expected from a SWx support service, including its various modes of operations and time-critical parameters collaborated within the recognized ICAO working committee and ad hoc group, are provided in Appendix C. These ConOps requirements were developed by performing a functional analysis on the criticality of these needs. A ConOps is essentially a top-level narrative functional analysis. 1019 The complete set of functional requirements is presented in Appendix D for reference. 1020 5.2 1021 5.2.1 Existing Performance Requirements 1022 1023 1024 1025 No previous performance requirements exist for SWx information. These SWx information performance requirements are the first of their kind. This inaugural set of requirements is breaking new ground in an attempt to bring some continuity and standardization to operators, support personnel and management, and end users in executing global operations. 1026 5.2.2 New Performance Requirements 1027 1028 1029 1030 1031 1032 1033 1034 The goal of these threshold values was to improve the efficiency of the airline flight planning process and en route support in the case of dynamically changing SWx conditions and potential impacts to crew and passengers in maintaining safety and efficiency. The goal was to strike a balance between the right amount of pertinent SWx information, provided in a timely manner most useful to the airlines, and support for operators. This balance mitigates information overload during periods of very active SWx and dynamic changes in the weather criteria thresholds. End users need real-time information in useable format to make informed, creditable decisions to maintain safe and cost-effective operations for themselves and the customer. 1035 1036 Appendix C contains the threshold values and the necessary details from which more formal and extensive performance requirements can be developed in the future. 5.1 SPACE WEATHER REQUIREMENTS FOR AVIATION Functional Requirements Performance Requirements 23 OFCM/OSTP, Impacts of NPOESS Nunn-McCurdy Certification and Potential Loss of ACE Spacecraft Solar Wind Data on National Space Environmental Monitoring Capabilities (January 2008). 35 1037 6 OPERATIONAL SCENARIO 1038 1039 1040 1041 1042 It is envisioned that globally-harmonized SWx data and the categorization of SWx aviation sources follow a path similar to that of terrestrial weather, and that the decision on the data and categorization be agreed upon at the ICAO- and WMO-level. This work on aviation operations is being undertaken by the FAA (for ICAO), ISES, and the WMO and is proposed for wider consideration. 1043 1044 This section defines how SWx analysis capabilities can be used operationally. The usage scenarios are derived from the User Needs document, as well as the existing general ConOps. 1045 1046 1047 The CPWG sub-group used Chicago-to-Hong Kong polar route operations to consider what SWx information, observations, and forecasts are required for each of the impacted areas of the operation as shown in Figure 6. In Situ 1048 1049 1050 Figure 6: Phases of Flight 1051 1052 The SWx forecast will populate a consistent four-dimensional (4-D) grid of SWx information, covering the entire airspace traversed by the depicted trajectory. 1053 1054 1055 1056 1057 1058 1059 1060 1061 1062 Flight planning DSTs that are not an ICAO requirement can retrieve relevant information from this grid along the planned and alternative flight paths. This includes takeoff, through departure climb, cruising altitude, and the descent to landing. If any type of SWx hazard exceeds established risk tolerance levels anywhere along the flight path, the risk will be flagged by the DST. In some of the more sophisticated DSTs, not only will operators be notified of the SWx imposed hazard along a planned trajectory, but the DST will also generate alternate or optimized trajectories to minimize the operators’ risk. The challenge is that not all airlines have access to such tools, but the proportion of accessibility from airlines to utilize these safetyrelevant tools will continue to grow as shown in Figure 7. Scenarios are best-depicted with some form of graphical sequence ladder diagram to show a conceptual decision-making process. 36 Flight Planner Decision Support Tool Space Weather Sensor (Observations) 4-D Weather Grid Continuous Space Weather Model Data A Continuous B C D E G F H I 1063 1064 1065 Adverse Space Weather Event Occurs A 4-D SWx Grid Is Dynamically Updated With SWx Data G Adverse Space Weather Event Is Observed B 4-D SWx Grid Is Dynamically Updated With Model Data H Grid is populated with Adverse SWx Info C Planner Requests Weather Information I DST receives adverse SWx information D DST Queries 4-D Weather Grid E DST Returns SWx Information F Planner Receives SWx Information from 4-D Grid Figure 7: Ladder Sequence Diagram Showing How Operational Scenarios are Depicted 1066 1067 1068 1069 1070 1071 The following could become recommended actions if communications are forecast to be poor in some area for a period. The Airport Authority should: (1) reduce traffic flow, as appropriate, in response to the problem; (2) if the GNSS is going to be affected, issue a Notice to Airmen (NOTAM) to that effect (the aircraft operator’s Mandatory Minimum Equipment List will show whether flight is permitted without reliable GNSS); and (3) if a GNSS approach is planned at a destination or alternate, a NOTAM should be issued to raise the approach/landing minima. 1072 1073 1074 1075 1076 1077 1078 Because the 4-D grid is updated dynamically, these risk mitigation decisions are reassessed continuously, and the operator is only notified when established thresholds are reached during any of the flight segments shown in Figure 6. While these tolerance levels have not yet been established, a small group of subject matter experts are working to baseline these standards. There is discussion that the NOAA Space Weather Scales serve as the starting point for classifying the radio frequencies impacted by the solar event. DST mechanisms for flight planning will need a consistent, appropriately-scaled, and dynamically-updated 4-D grid of SWx 37 1079 1080 1081 1082 1083 1084 1085 1086 hazard probabilities from which to draw information. More details on risk levels will be matured once the operational and functional requirements have been established and the scientific capabilities are in place to enable threshold-specific performance requirements to be further matured when technological capabilities can routinely be achieved (sometime after implementation into the ICAO Weather Annex 3). If the derivative products from some authorized provider (MWO, RWC, etc.; and yet to be determined) are to be included as an official product in Annex 3, proper arrangement should be made for dissemination of such information to the appropriate authorized provider. 1087 7 1088 1089 There are several benefits to implementing global standards for the provision and use of SWx information. These positive impacts include: 1090 1091 1092 1093 1094 1095 1096 1097 1098 1099 1100 SUMMARY OF IMPACTS Improved SWx event analysis and forecast information Improved dissemination of information about SWx events affecting international air navigation Improved flight planning to avoid the impacts of SWx events Improved en route avoidance of SWx events by flight crews This will result in maximum utilization of polar routes which improves the efficiency of international flight operations and provides cost savings to the airline industry. In addition, safety of flight will be improved through a reduction in potential encounters with SWx phenomena that can degrade the performance of aircraft communications and navigation systems. 1101 1102 38 APPENDIX A: MATERIAL LIST OF REFERENCES The footnote references throughout this document that describe SWx impacts on aviation operations are listed by number in the table below. Table 8: Reference List # ABBR 1 NSWP 2 ISWOF 3 JPDO 4 OFCM Phase I 5 WMO 6 CPWG 7 FAA 8 SWPC 9 10 SWPC SWPC 11 UAL 12 USGS 13 ICAO 14 ICAO 15 ICAO 16 ICAO 17 18 ICAO ICAO 19 NASA 20 21 22 DOT CFR Website 23 MIT/LL DOCUMENT TITLE Report of the Assessment Committee for the National Space Weather Program, FCM-R242006, Office of the Federal Coordinator for Meteorological (OFCM) Services and Supporting Research (June 2006). Integrating Space Weather Observations& Forecasts into Aviation Operations, American Meteorological Society (AMS) & SolarMetrics, Policy Workshop Report (March 2007) www.ametsoc.org/atmospolicy. Four-Dimensional Wx Functional Requirements for NextGen Air Traffic Management, JPDO Weather Functional Requirements Study Group, Version 0.2 (15 February 2008). OFCM/OSTP. Impacts of NPOESS Nunn-McCurdy Certification and Potential Loss of ACE Spacecraft Solar Wind Data on National Space Environmental Monitoring Capabilities (January 2008). WMO Space Programme SP-5, The Potential Role of WMO in Space Weather (April 2008). Space Weather Sub-Group of the Cross Polar Working Group, Integrating Space Weather Observations & Forecasts into Aviation Operations, Aviation Space Weather User Requirements, Version 3.02 (November 2010). Michael Stills, United Airlines, in support of FAA Concept of Operations for International SWx Information, presentation at the AMS 9th Symposium on SWx (January 2012). NOAA, Space Weather Prediction Center (SWPC), Manual on Space Weather Effects in Regard to International Air Navigation (January 2011). SWPC Website: www.swpc.noaa.gov (Alert/Warnings). SWPC Website: www.swpc.noaa.gov/NOAAScales. Michael Stills, United Airlines, Polar Operations and Space Weather, presentation to the Space Weather Enterprise Forum (SWEF) (21 June 2011). Dr. Jeffrey J Love, USGS, 91st Annual AMS Conference, 8th Symposium on Space Weather, (January 2011). ICAO Annex 2, Rules of the Air, To the Convention on International Civil Aviation, Chapter 3, Ninth Edition (July 1990). ICAO Annex 3, World Area International Air Navigation, Chapter 3, Meteorological Watch Offices, Appendix 2, WAFS, 17th Edition (July 2010). ICAO Annex 6, Chapters 6 and 12. ICAO Annex 10, Aeronautical Telecommunications, Chapter 4, Aeronautical Fixed Services, 6th Edition (October 2001). Annex 11, Chapter 6, Air Traffic Services Requirements for Communications, para 6.1.2.2. Document 4444, Chapter 15, paragraph 15. 5.4, for Descents due to Solar Cosmic Radiation. Dr. Christopher J. Mertens, Principal Investigator, NAIRAS 2009 Annual Report, NASA Langley Research Center, Hampton, VA. Office of Aerospace Medicine, Washington, DC, DOT/FAA/AM-03/16 (October 2003). Code of Federal Regulations (CFR) Title 14 (Aeronautics and Space). http://encyclopedia.thefreedictionary.com/Heliosphere Massachusetts Institute of Technology, Lincoln Laboratory website http://www.ll.mit.edu/mission/aviation/wxatmintegration/usedecisionsupport.html A-1 APPENDIX B: DEFINITIONS 4-D Grid A virtual, four-dimensional geographical coordinated grid of weather data information not located in one single physical location linked to real-time enabling network for simultaneous, reliable and secured connectivity. ACE NASA research satellite monitoring the space environment (solar wind) beyond the Earth’s magnetic field along the Sun-Earth angle, one and one-half million kilometers out in space at a point of equal gravitational equilibrium. DST24 Use of Integrated Weather-ATM Decision Support Systems provides some interesting challenges in development and benefits assessment because there is a mixture of aviation weather product development and explicit modeling of some aspects of the aviation system itself. Conventional Approach to Aviation Decision Making In the “conventional” approach to aviation decision making, the human users must determine the impact of the weather on the ATC system before a decision can be made. If DSTs (see Figure 8), such as the Cooperative Route Coordination Tool (CRCT) in the Enhanced Traffic Management System (ETMS), are used to aid in the execution of the conventional operational decision loop, the user must provide results from the impact assessment phase (e.g., Flow Constrained Areas) to the tools in order to take advantage of the decision guidance they provide. Although this approach has been successful in a number of specific applications, it is becoming clear that it is not adequate overall, since often the task of determining the weather impact manually can be extremely difficult. 24 Massachusetts Institute of Technology, Lincoln Laboratory website http://www.ll.mit.edu/mission/aviation/wxatmintegration/usedecisionsupport.html B-1 Overall convective weather impact mitigation process. The TMU workload associated with convective weather management includes all five elements shown in the “operational decision loop.” event reports GBAS It supports all phases of approach, landing, departure, and surface operations within its area of coverage. The current ILS suffers from a number of technical limitations such as VHF interference, multipath effects (for example, due to new building works at and around airports), as well as ILS channel limitations. GBAS is expected to play a key role in maintaining existing all-weather operations capabilities at different flight supporting airports. GBAS is seen as a necessary step toward the more stringent operations required at airports supporting precision approach and landing. HELIOSPHERE25 The heliosphere is a bubble in space “blown" into the instellar medium (the hydrogen and helium gas that permeates the galaxy) by the solar wind. Although electrically neutral atoms from interstellar volume can penetrate this bubble, virtually all of the material in the heliosphere emanates from the Sun itself. For the first ten billion kilometers of its radius, the solar wind travels at over a million km per 25 http://encyclopedia.thefreedictionary.com/Heliosphere B-2 hour. As it begins to drop out with the instellar medium, it slows down before finally ceasing altogether. The point where the solar wind slows down is the termination shock; the point where the interstellar medium and solar wind pressures balance is called the heliopause; the point where the interstellar medium, traveling in the opposite direction, slows down as it collides with the heliosphere is the bow shock. The solar wind consists of particles, ionized atoms from the solar corona, and fields, in particular magnetic fields. As the Sun rotates once in approximately 27 days, the magnetic field transported by the solar wind gets wrapped into a spiral. Variations in the Sun's magnetic field are carried outward by the solar wind and can produce magnetic storms in the Earth's own magnetosphere. The heliospheric current sheet is a ripple in the heliosphere created by the Sun's rotating magnetic field. Extending throughout the heliosphere, it is considered the largest structure in the B-3 Solar System and is said to resemble a "ballerina's skirt" produce magnetic storms in the Earth's own magnetosphere. The heliosphere's outer structure is determined by the interactions between the solar wind and the winds of interstellar space. The solar wind streams away from the Sun in all directions at speeds of several hundred km/s (about 1,000,000 mph) in the Earth's vicinity. At some distance from the Sun, well beyond the orbit of Neptune, this supersonic wind must slow down to meet the gases in the instellar medium. B-4 B-5 L1 A location on the Sun-Earth line where gravitational forces can be balanced to maintain a stable orbit. Approximately 1.5 million miles upstream of the Earth. Solar wind monitors located there allow a 20-60 minute (depending on solar wind velocity) warning of geomagnetic disturbances at Earth. NAIRAS26 The Nowcast of Atmospheric Ionizing Radiation for Aviation Safety (NAIRAS) model is a prototype operational model currently under development in the United States at the National Aeronautics and Space Administration (NASA), Langley Research Center. The NAIRAS model provides global, real-time, data-driven predictions of atmospheric ionizing radiation exposure for archiving and assessing the biologically harmful radiation levels at commercial airline altitudes. The sources of ionizing radiation are Galactic Cosmic Rays (GCR) and Solar Energetic Particle (SEP) events, which can accompany disturbances on the Sun’s surface. The composition and energy spectra of atmospheric ionizing radiation originate from and are subject to variability in SWx phenomena. As such, the NAIRAS model provides a SWx DST related to radiation impacts on crew and passengers of long-haul aircraft, an area of national priority for NASA’s Applied Science Program. The key NAIRAS data products are global distributions of vertical profiles of radiation exposure rates, computed from the Earth’s surface to approximately 100 km in real time. NAIRAS output will be made available at NOAA’s National Weather Service’s, Aviation Digital Data Service (ADDS). NOAA/ADDS is a decision support system whereby NAIRAS results can provide a tool for commercial airlines and aircrew to monitor current and accumulated radiation exposure. The long-term goal is to transition the prototype NAIRAS model into an operational system that will be adopted by NOAA/SWPC. 26 Dr. Christopher J. Mertens, Principal Investigator, NAIRAS 2009 Annual Report, NASA Langley Research Center, Hampton, Va. B-6 PCA An anomalous condition of the polar ionosphere where HF and VHF (3-300 MHz) radiowaves are absorbed, and LF and VLF (3-300 kHz) radiowaves are reflected at lower altitudes than normal. PCAs generally originate with major solar flares, beginning within a few hours of the event and maximizing within a day or two of onset. As measured by a riometer, the PCA event threshold is 2 dB of absorption at 30MIlz for daytime and 0.5 dB at night. In practice, the absorption is inferred from the proton flux at energies greater than 10 MeV, so that PCAs and proton events are simultaneous. However, the transpolar radio paths may be disturbed for days, up to weeks, following the end of a proton event. RIOMETERS The word riometer stands for Relative Ionospheric Opacity Meter. Riometers measure the strength of radio noise originating from stars or galaxies and arriving at the earth after passing through the ionosphere. A riometer is a passive scientific instrument used to observe ionospheric absorption, particularly absorption at altitudes less than 110 km caused by electron precipitation. The sky is filled with stars and galaxies that emit a broad spectrum of radio noise and the noise is strong enough to be picked up using sensitive receiving equipment. Because some regions of the sky are noisier than others, this noise varies on a predictable basis as the Earth rotates. Although noise due to stars or galaxies may change over very long time frames, it is constant enough to be considered a repeatable function of Local Sidereal Time. RNP Required Navigation Performance is a type of Performance-Based Navigation (PBN) that allows an aircraft to fly a specific path between two three-dimensionally defined points in space. A navigation specification that includes a requirement for on-board navigation performance monitoring and alerting is referred to as an RNP specification. An RNP of .3 means the aircraft navigation system calculates its position to within a circle radius of 3/10 of a nautical mile. SOHO A joint NASA/ESA (European Space Agency) research satellite with instrumentation to measure the Sun to predict solar flare activity. TEC The Solar EUV and Lyman alpha emissions create the ionosphere by photo-ionization, which ionizes neutral atoms and molecules producing free ions and electrons. The Total Electron Content (TEC) of these positively and negatively charged particles embedded in the neutral atmosphere form weak plasma that interacts with radio waves of various frequencies in different ways. B-7 APPENDIX C: FUNCTIONAL AND PERFORMANCE REQUIREMENTS Functional Set of Space Weather Information Requirements Operational Requirement Space Weather conditions information shall be provided to all Stakeholders. Space Weather conditions information shall be delivered to all Stakeholders. Functional Requirement Space Weather Information shall be provided by an ANSP: 1. The infrastructure to deliver observed space weather information. 2. The infrastructure to deliver solar radiation storm observations and forecasts. 3. The infrastructure to deliver geomagnetic storm observations and forecasts. 4. The infrastructure to deliver radio blackout event (solar flare) observations and forecasts. 5. The infrastructure to deliver galactic cosmic ray observations and forecasts. 6. The infrastructure to deliver ionospheric activity observations. Operational Requirement To provide knowledgeable understanding of current and space weather conditions. To provide information on current and space weather conditions. Space Weather conditions shall be observed: Space Weather conditions shall be observed. 1. Shall observe geomagnetic storms.2. Shall observe solar radiation storms. 2. Shall observe radio blackout (solar flare) events. 3. Shall observe galactic cosmic rays 4. Shall observe ionospheric activity. To provide knowledgeable understanding of current space weather conditions. Space Weather conditions shall be forecast: Space Weather conditions shall be forecast. 1. Shall forecast geomagnetic storms. 2. Shall forecast solar radiation storms. 3. Shall forecast radio blackout (solar flare) events. 4. Shall forecast galactic cosmic rays C-1 To provide knowledgeable understanding of forecast space weather conditions. 1. Space weather information required from all available sources by the end users shall be acquired for a Post-event Analysis (PEA). Post-Event Analysis shall be performed. Space weather impacts shall be defined. a. Space weather information shall be collect by service-providing organizations. b. Operational response information shall be collect by the airlines. c. The space weather related impact shall be analyzed through some postevent analysis. d. Analysis results shall be use to improve space weather situational awareness. 1. Space weather impacts on aviation operations will be defined. 2. Aviation operators shall define space weather impacts. C-2 To improve knowledge of space weather cause and effect. To improve knowledge of space weather impacts on aviation. Operational Requirement Space Weather Impacts resulting in the disruption to or loss of HighFrequency (HF) communications shall be defined. Space Weather Impacts resulting in the disruption to or loss of Very High-Frequency (VHF) communications shall be defined. Space Weather Impacts resulting in the disruption to or loss of Ultra High-Frequency (UHF) communications shall be defined. Space weather impacts resulting in the disruption to or loss of satellite communications shall be defined. Functional Requirement Space weather impacts shall be defined for the disruption to or loss of HighFrequency (HF) communications. Space weather impacts shall be defined for the disruption to or loss of Very HighFrequency (VHF) communications. Space weather impacts shall be defined for the disruption to or loss of Utra HighFrequency (UHF) communications. Space weather impacts shall be defined for the disruption to or loss of satellite communications. C-3 Reason for Requirements Ability to make position reports and remain compliant within the confines of ICAO Annex 11 paragraph 6.1.2.2 and CFR 14, § 121.99 in the mid and low latitudes (dayside), polar regions, and auroral latitudes from geo-magnetic storms related severe weather events: Solar Extreme Ultra-Violet (EUV) or Solar X-rays during flares, Solar Particle Events (SPE), and Geomagnetic Storms. Ability to make accurate position reports and remain compliant within the confines of ICAO Annex 11 paragraph 6.1.2.2 and CFR 14, § 121.99 on the sunlight side due solar radio noise. Ability to make position reports and remain compliant globally within the confines of ICAO Annex 11 paragraph 6.1.2.2 and CFR 14, § 121.99 due to geomagnetic storms. Ability to make position reports and remain compliant globally within the confines of ICAO Annex 11 paragraph 6.1.2.2 and CFR 14, § 121.99 due to geomagnetic storms. Operational Requirement Space weather impacts resulting in variations on radiation that produce: a. erroneous measurements on onboard avionics b. limit effects on humans (accumulative exposure amounts over time) The impacts of space weather affecting the reliance of GNSS are defined. Space weather warnings shall be generated. Space weather alerts shall be generated. Space weather updates shall be generated. Functional Requirement 1. The impacts of variations in radiation that produce erroneous measurements from onboard avionics shall be defined. 2. Take action to adjust altitude to limit radiation exposure dosage potential to aircrew and passenger. The impact of space weather on the reliability of the GNSS (percentage of interruption time) availability shall be defined from appropriate satellite navigation authorities as already performed in some regions (i.e.; the FAA Satellite Navigation Services in the United States) via a NOTAM. 1. Space weather warnings shall be generated containing a lead time of six hours and essentially determined by a parameter forecast value to exceeding the next userspecified threshold level. 2. Space weather alerts shall be generated when the activity is forecast to remain above the parameter actionable level, essentially determined by a forecast value that continues to exceed the user-specified operational threshold and forecast time of cessation. 3. Space weather updates shall be generated when the parameter value is forecast to decrease below the parameter actionable level or operational threshold. C-4 Reason for Requirements Ability to measure radiation doses of ionizing radiation energy > 100 MeV for flights routes in Polar/High latitude regions at high altitudes for aircraft, Reusable Launch Vehicles (RLVs) and Expendable Launch Vehicles (ELVs) effected by Galactic Cosmic Rays (GCR), Solar Cycle, and Solar Proton Events (SPE). Ability to accurately determine and predict occurrences of ionospheric scintillation and solar radio burst to analysis the liability of the positioning information used for navigation, approach and landing due to signal loss and allow for the utilization of alternative methods in the equatorial and auroral regions for solar EUV during flares, Geomagnetic Storms, and SPEs. To provide more clear description of space weather information regarding its expected severity to improve aviation operational efficiency. Space Weather Information for observations define the current space weather conditions, not just of the Sun but its activity source, and the cause and effect where the impact takes place. Operational Requirement Functional Requirement Reason for Requirements The future space weather conditions shall be described by specifying the time of the condition in minutes, hours, or days in advance of the space weather impact aviation industry-specified. To provide future operations impacts along flight route with confident accuracy and allow cost effective tactical and strategic flight planning to maximize efficiency while maintaining safety. Space weather conditions shall be forecast with a user-specified update rate. Space weather conditions shall be forecast with a user-specified latency. Space weather conditions shall be forecast with a user-specified temporal increment. Space weather climatology shall be generated. Space weather observations and forecasts shall be reported in a standardized user-specified text format. Space weather information graphical analysis charts shall depict significant Space weather across all defined flight boundary regions. Space weather information shall be delivered using all available delivery methods. 1. 2. 3. 4. 5. Scintillation climatology shall be generated. Solar cycle climatology shall be generated. Geomagnetic storm climatology shall be generated. Solar radiation intensity climatology shall be generated. High energy charged particle climatology for magnetic latitude regions shall be generated. Space weather reports shall be standardized in user-specified formats: 1. Space Weather information formats shall include graphical analysis charts of space weather observations. 2. Space Weather information formats shall include textual space weather observations. 3. Space Weather information shall be translated from standard formats into local dialects. 1. All space weather information graphical analysis charts shall depict significant Space weather across all defined flight boundary regions. 2. Space weather information shall be delivered by adequate available delivery methods to reach end user in timely manner for effective risk avoidance. 3. Flight magnetic latitude regions shall be identified with expected durations of impact from space weather hazards in corresponding reports. 4. Graphical analysis charts shall use standardize color schemes or shadings in graphical reports similar to traffic light scheme used to define the distribution of the space weather event severity based on performances by a nominal airframe with typical flight deck equipage and instrumentation. C-5 Used to interpret the type of phenomena over time in support of post event analysis of commercial, operational, safety and technological impacts. To mitigate cost of redundant infrastructure and establishing a global standard for global harmonization in format and content consistency. To mitigate cost of redundant infrastructure and establishing a global standard for global harmonization in format and content consistency. Operational Requirement Space weather information shall be standardized in format and content within the reports and in line with ICAO Annex 3 templates and requirements. The severity of space weather impacts contained in the reports for text and graphical displays to be described in ICAO Annex 3. The severity of space weather impacts contained in the reports for text and graphical displays shall follow ICAO Annex 3 templates and requirements. Functional Requirement 1. 2. 3. 4. 5. All space weather reports shall be specified the station identifiers. All space weather reports shall specify the affected airspace or solar regions. All space weather reports shall follow standardized formats. All space weather reports shall use defined boundaries of the solar regions. All space weather reports shall specify the date and time of the report in coordinated universal time (UTC). 6. All space weather reports shall comply with the ICAO Annex 3 templates. 7. All space weather reports shall comply with the ICAO Annex 3 requirements. 1. Space weather terminology shall be defined. 2. Standardize space weather terminology shall be defined. 3. Severity of impact in a standardized format in the space weather reports for text and graphical displays shall be included. 4. The cause of the space weather hazard in space weather reports shall be specified. 5. The altitudes or flight levels of the hazard in space weather reports shall be specified. 6. A standardized international severity storm index scale such as the NOAA Space Weather Storm Scale shall be established and be used in describing the severity index of the event and related impact. 7. The color schemes or shading (i.e.; traffic light system – red, yellow, green) in graphical reports that are used to define the distribution of the space weather event severity shall be standardized. 8. The standardized international severity storm scale index shall be in-line with ICAO Annex 3 templates. 9. The standardized international severity storm scale index shall be in-line with ICAO Annex 3 requirements. C-6 Reason for Requirements Developing a consistency in the content of message that embraces global harmonization in a global standard. Developing a consistency in the content of message that embraces global harmonization in a global standard. Operational Requirement Space weather information timelines and durations shall be described for both text reports and graphical charts (i.e.; forecast, warning, alert, and update). Space weather timelines and duration shall be similar to terrestrial weather. Space weather information accuracy estimates shall be provided. Functional Requirement Reason for Requirements The following information as warranted in all Forecast, Warnings, Alerts and Update type messages shall include: 1. The applicable impact shall be defined. 2. The “from” validation time to include day of month shall be specified. 3. The “duration” of event or valid “to” time shall be specified. 4. Ongoing changes during the event shall be provided. 5. A space weather forecast shall be provided at the 4-synoptic times daily out to the 30-hour timeframe. 6. A space weather 30-hour forecast shall be provided every 6-hours. 7. For text message reports only, 30-hour Space Weather forecast shall be provided every six hours unless conditions more warrant frequent updates. 8. Space weather forecast shall be provided daily for 3-Day and 7-Day time frames. 9. “Warnings” for space weather impacts shall be provided with six-hour lead time. 10. “Text” message reports for six-hour warning shall be provided describing any Severe weather element forecast that increases the hazard index severity in accordance to NOAA Space Weather Scale or another established international severity index scale. 11. “Alert” messages shall be immediately delivered. 11a. “Alert” messages shall be valid for a specific time period where the activity is forecast to remain above a specified threshold or will increase further based upon the NOAA Space Weather Storm Scale or another established international severity index scale. 12. “Update” messages as warranted shall be delivered in a manner described for “Alert” messages but for the parameter changes where the space weather event activity decreases below actionable levels. These messages establish global harmonization of space weather information in a standardized manner that reduces ambiguities while enhancing operator efficiency over long-haul routes. The space weather information with the accuracy shall be delivered as follows: 1. The space weather information shall state the reliability, percentage (%) confidence levels or probability of information (alert/event/parameter, change, etc.) occurring within the defined time frame of the report/graphic. 2. The accuracy or % confidence levels established for various hazards (not standardized) is defined with current condition remarks supporting reliability targets. 3. The space weather information provider shall use simple, plain language similar to terrestrial reporting to describe familiar terminology for space weather events in any of the current and accepted message format to include duration of the phenomena in hours as changes warranted in space weather conditions causing or lifting operational impacts. Advocates global harmonization of space weather information in single global standard. C-7 Operational Requirement Functional Requirement Reason for Requirements The geomagnetic latitudes corresponding to geographical delineated regions affected by space weather shall be defined across aviation global airspace tied to latitudinal geographical regions: Polar Cap, Auroral Electrojet, Middle-Latitude, Ring Current, and Equatorial Electrojet. The geomagnetic geographic latitude boundaries (Appendix G) and volumes affected by the hazards within the report shall be defined: 1. The latitude and longitude shall be defined. 2. The Flight Information Regions (FIRs) shall be defined. 3. The ISE Regional Warning Centers (RWCs) regions shall be defined. 4. The altitudes/flight levels shall be defined. Space weather events are generally global in nature but depending on the type of solar storm its severity index impact vary within defined banded aviation airspaces around the world requiring various mitigating operational actions to maintain maximum efficiency. Space weather information, reports, and charts shall be transmitted via all currently available regulatoryapproved transmission methods. Current aviation weather information transmission methods shall be utilized and integrate with aviation operations in a similar manner to terrestrial weather whenever possible: 1. Space weather information shall be transmitted via a qualified internet communications Provider. 2. The text and chart reports shall be integrated with dispatch for forecast, warnings, alerts and updates. 3. Audio-visual or “attention getters” reports associated with warnings, alerts and updates for dispatchers shall be provided. Using available and already established infrastructure that is already familiar to the operator will mitigate cost to the industry and confusion when integrating this new type of information into the system for coordinated en route avoidance maneuvers and more efficient flight planning. C-8 Operational Requirement The observed effects on disruptions to HF communications and forecast shall be provided to all stakeholders. Functional Requirement 1. The severity of the solar event to HF disruption shall be quantified as set forth in the NOAA Space Weather Storm Scale or an established international severity index scale. 2. The related information based upon the severity on signal strength/loss, clarity and available or best useable frequencies shall be provided. 3. The timelines and durations of HF disruption with the following information shall be defined: a. A “valid from” time frame shall be provided b. A duration or “ valid to” time frame shall be provided c. Ongoing changes shall be provided as part of any Update Report d. Any “confidence levels” shall be provided e. Current condition reports shall be provided 4. The forecast accuracy for HF disruption in a text or graphic report shall be defined. a. In 2016, space weather forecast conditions shall meet the defined reliability percentage (%) confidence levels for these timeframes and types of reports: 1. 7 days – 45% 2. 3 days – 55% 3. 30 hours – 65% 4. Warnings – 75% 5. Alerts – 75% 6. Updates – 75% 7. PEA – 99% 5. The geomagnetic geographic latitude region(s) defined in Appendix G (Figure 9) for the HF disruption shall be recognized in regard to their products and service messages. C-9 Reason for Requirements To maximize operational efficiency and cost benefit for the aviation industry through global harmonization of space weather information delivered in a global standard framework. Operational Requirement The observations of disruptions to VHF communications from space weather events (from Sudden Ionospheric Disturbance [SID] of radio signals) occurring on the sunlit side of the Earth shall be provided. SID duration shall be forecast in minutes and hours. Functional Requirement 1. The severity of the solar event to VHF disruption shall be quantified as set forth in the NOAA Space Weather Storm Scale or an established international severity index scale. 2. The related information based upon the severity on signal strength/loss, clarity and available or best useable frequencies shall be provided. 3. The timelines and durations of VHF disruption shall be defined with the following information: a. A “valid from” time frame shall be provided b. A duration or “ valid to” time frame shall be provided c. Ongoing changes shall be provided as part of any Update Report d. Any “confidence levels” shall be provided e. Current condition reports shall be provided 4. The forecast accuracy for VHF disruption shall be defined in a text or graphic report. a. In 2016, space weather forecast conditions shall meet the defined reliability percentage (%) confidence levels for these timeframes and types of reports: 1. 30 hours - 65% 2. Warnings – 75% 3. Alerts – 75% 4. Updates – 75% 5. PEA – 99% 5. The geomagnetic geographic latitude region(s) defined in Appendix G (Figure 9) for the VHF disruption shall be recognized in regard to their products and service messages. C-10 Reason for Requirements To maximize operational efficiency and cost benefit for the aviation industry through global harmonization of Space Weather information delivered in a global standard framework. Operational Requirement The observations, forecasts and descriptions of impact on a line-ofsight signal loss to UHF communications shall be provided to all stakeholders. The line-of-sight signal loss to UHF communications duration shall be forecast in minutes and hours. Functional Requirement 1. The severity of the solar event to UHF disruption shall be quantified as set forth in the NOAA SWx Storm Scale or an established international severity index scale. 2. The related information based upon the severity on signal strength/loss, clarity and available or best useable frequencies shall be provided. 3. The timelines and durations of UHF disruption shall be defined with the following information: a. A “valid from” time frame shall be provided b. A duration or “ valid to” time frame shall be provided c. Ongoing changes shall be provided as part of any Update Report d. Any “confidence levels” shall be provided e. Current condition reports shall be provided 4. The forecast accuracy for UHF disruption shall be defined in a text or graphic report. a. In 2016, space weather forecast conditions shall meet the defined reliability percentage (%) confidence levels for these timeframes and types of reports: 1. 7 days - 45% 2. 3 days - 55% 3. 30 hours - 65% 4. Warnings – 75% 5. Alerts – 75% 6. Updates – 75% 7. PEA – 99% 5. The geomagnetic geographic latitude region(s) defined in Appendix G (Figure 9) for the UHF disruption shall be recognized in regard to their products and service messages. C-11 Reason for Requirements To maximize operational efficiency and cost benefit for the aviation industry through global harmonization of Space Weather information delivered in a global standard framework. Operational Requirement The observations and a description of impact of the observed effects on a line-of-sight signal loss to VHF/UHF communications to the satellite (classified as satellite communications) shall be provided. The line-of-sight signal loss to UHF communications duration shall be forecast in minutes and hours. Functional Requirement 1. The severity of the solar event to satellite communication disruption shall be quantified as set forth in the NOAA Storm Scale or an established international severity index scale. 2. The related information based upon the severity on signal strength/loss, clarity and available or best useable frequencies shall be provided. 3. The timelines and durations of satellite communication disruption shall be defined with the following information: a. A “valid from” time frame shall be provided b. A duration or “ valid to” time frame shall be provided c. Ongoing changes shall be provided as part of any Update Report d. Any “confidence levels” shall be provided e. Current condition reports shall be provided 4. The forecast accuracy for satellite communication disruption shall be defined in a text or graphic report. a. In 2016, space weather forecast conditions shall meet the defined reliability percentage (%) confidence levels for these timeframes and types of reports: 1. 30 hours - 65% 2. Warnings – 75% 3. Alerts – 75% 4. Updates – 75% 5. PEA – 99% 5. The geomagnetic geographic latitude region(s) defined in Appendix G (Figure 9) for the satellite communication disruption shall be recognized in regard to their products and service messages. C-12 Reason for Requirements To maximize operational efficiency and cost benefit for the aviation industry through global harmonization of space weather information delivered in a global standard framework. Operational Requirement Observations and forecasts of radiation environment that affect avionics shall be provided to all stakeholders. Space weather shall be delivered to all appropriate operational and Air Traffic Management (ATM) decision-makers using a decisionmaker matrix based upon similar criteria for Preliminary Performance Requirements formulated for the United State’s NextGen arena Functional Requirement Reason for Requirements 1. The related information of Galactic Cosmic Ray (GCR) rates shall be provided that will affect the aircraft avionics. 2. The solar radiation rates shall be provided that will affect the aircraft avionics. 3. The rate of change of the radiation environment rates (up or down) shall be provided that will affect the aircraft avionics. 4. The peak radiation rates shall be provided that will affect the aircraft avionics. 5. The risk factor shall be provided on the aircraft avionics. 6. The high energy (ionized) particle spectra shall be provided for Post-Event Analysis affecting aircraft avionics. 7. The timelines and durations of the radiation effects shall be provided with the following information: a. A “valid from” time frame shall be provided b. A duration or “ valid to” time frame shall be provided c. Ongoing changes shall be provided as part of any Update Report d. Any “confidence levels” shall be provided e. Current condition reports shall be provided 8. The forecast accuracy of the radiation effects shall be provided in a reliability percentage (%) confidence levels for future text or graphic reports: 1. 7 days - 45% 2. 3 days - 55% 3. 30 hours - 65% 4. Warnings – 75% 5. Alerts – 75% 6. Updates – 75% 8. PEA – 99% To maximize operational efficiency and cost benefit for the aviation industry through global harmonization of space weather information delivered in a global standard framework. 1. The a matrix of space information types to all aviation decision-makers shall be provided as recognized in Section 4.5 (Table 7). 2. The international aviation operators to develop a decision-maker matrix similar to Section 4.5 (Table 7) shall be coordinated for future aviation operations. To maximize operational efficiency and cost benefit for the aviation industry through global harmonization of space weather information delivered in a global standard framework. C-13 Operational Requirement Functional Requirement Reason for Requirements The method and delivery path of well-defined regulated, and clearly understood daily space weather pilot briefing packs shall be provided using similar practices and protocol already established for terrestrial weather information. 1. The seamless integration of space weather pilot briefing packs shall be advocated into the operational routine. 1a. The space weather information availability shall be ensured to all decisionmakers at all management/user levels throughout the aviation industry. 2. The current methods of communicating aviation-related terrestrial weather information shall be used when possible to ensure the information is timely, standardized and consistent with aviation operational processes. 3. The space weather aviation information shall be integrated into the normal flight planning and the terrestrial briefing weather packs for all pilots, dispatchers and Air Traffic Control (ATC) personnel. To assist in educating the pilots on blending space weather impacts with terrestrial hazardous and help improve their strategic and tactical flight planning in maximizing operational efficiency and cost benefit for the aviation industry through global harmonization of space weather information delivered in a global standard framework. Space weather information education and training shall be integrated into operators, agencies and unions, education and training programs. 1. An educational and training program shall be developed for a basic understanding of the science and the terminology of space weather. 2. The space weather scientific education materials shall be developed on the impacts of space weather on aviation operations. 3. The institutionalization of training programs at all levels to dispatchers, aircrews, ATC personnel and meteorologists shall be advocated. 4. The materials in these programs shall be ensured they are standardized by operation. 5. The standardization of space weather education and training material implemented in training programs shall be ensured by aviation operators. To ensure pilots, and all air traffic management receive the necessary education and uniform training required to better understand space weather impacts on aviation operations, which will improve all phases of the operations from flight planning to coordinating seamless alternative maneuvers, in maximizing operational efficiency and cost benefit for the aviation industry through global harmonization of space weather information delivered in a global standard framework. The aviation community shall coordinate globally to standardize space weather information is delivery and use for operations. 1. Space weather information shall be standardized. 2. The new and improved space weather information shall be standardized. 3. The aviation industry on space weather information shall be coordinated to ensure data providers receive effective guidance on global standards. 4. The current terrestrial weather providers to support configuring space weather information and services shall be coordinated in a similar standardized fashion for delivery. 5. The space weather information and services shall be ensured to follow similar standardization protocols regulated by classification, type and source. Ensure space weather information and data providers work with current terrestrial weather providers to seamlessly configure new space weather information and service in a similar standardized manner for delivery as part of global harmonization in a single global standard. C-14 APPENDIX C (continued) Draft Performance Criteria Tables for Space Weather Obs and Forecast Products (See Notes Below) Accuracy, Thresholds for Observations and Forecasts Periods and Rates for Forecast Products (Note 1, 2) (Note 2) Geomagnetic Storms NOAA Space Weather Scale for Geomagnetic Storms G1 through G5 30 hr fcst 4X day plus amendments 3/7 day fcst 1Xday Solar Radiation Storms NOAA Space Weather Scale for Solar Radiation Storms S1 through S5 30 hr fcst 4X day plus amendments 3/7 day fcst 1Xday Galactic Cosmic Rays Particles greater than or equal to100 MeV; 10% above background 30 hr fcst 4X day plus amendments 3/7 day fcst 1Xday Radio Blackouts (Solar Flares) NOAA Space Weather Scale for Radio Blackouts R1 through R5 30 hr fcst 4X day plus amendments 3/7 day fcst 1Xday Element Verification, Confidence Level Latency (Note 4) Notes (includes data values associated with space weather scale thresholds, as applicable) (Note 3) Ionospheric Activity Total Electron Content Auroral Activity Estimate Baseline TBD 2025 values: FCSTS 7 days - 65% 3 days - 75% 30 hrs - 85% 6 hrs - 95% OBS Alerts - 95% 2016 values: FCSTS 7 days - 45% 3 days - 55% 30 hrs - 65% 6 hrs - 75% OBS Alerts - 75% K-index of 5, 6, 7, 8, 9 ≤ 1 min for Alert/Obs ≤ 15 minutes for forecasts This is not currently covered by a Space Weather Scale. Character of the alert/update/warning TBD. X-Ray Flux exceeded 10-5 ,5x10-5 , 10-4, 10-3, 2x10-3 W·m-2 Analysis 15 minute update interval +/- 6 TEC units ≤ 15 min Analysis 90 minute update interval +/- 50 km ≤ 15 min C-15 Proton Event 10 MeV Integral Flux exceeded 10pfu, 100pfu, 1000pfu, 10000pfu, 100000pfu Vertical TEC product NA Global D-Region Absorption Prediction Analysis based upon proton and X-ray flux 5 minute update interval (D-RAP) Proton Flux Estimated Planetary (proton and X-Ray flux accuracies 1 min D-RAP2 product apply) Flux .≥10, ≥100 MeV, 10 minute update interval +/-25% 1 min solar radiation storm data Analysis 3-hourly update interval TBD 5 min geomagnetic storm data 5 min averages in Watts/m2 5 minute update interval +/- 10% 5 min radio blackout event data K-Index X-Ray Flux C-16 Note1. Currently, an Alert is a special observation when a space weather element or scale number has passed above a threshold level. It currently includes a duration which states the time remaining at or above that level. Currently, a summary message indicates that the space weather element or scale number has passed below a threshold level. Note 2. Thresholds are generally the space weather scale numerical values (except in the case of galactic cosmic rays). Thresholds apply to both observations and forecast-type products, including forecasts that will be amended. The thresholds, in effect, become the amendment criteria. Note 3. Confidence percentages (referred to as verification percentages in performance requirements) are currently referenced as either 2016 or 2025. Baseline confidence/verification is currently being developed. User Needs document specified a 6-hour lead time on forecast threshold passage, 6-hour forecast is also referred to as a "warning." Note 4. Latency values are currently being defined. Current definition for latency as used in this table: elapsed time from data acquisition until delivery of data to the user (Latest time by which an element can be delivered and still useful to the customer). C-17 Space Weather Functional Requirements (FR) Tied to Specific Performance Requirements (PR) for Observation and Forecast Observations Forecasts 1.0 Space weather conditions shall be observed. FR 2.0 Space weather conditions shall be forecasted. 1.1 Geomagnetic storms shall be observed. FR 2.1 Geomagnetic storms shall be forecasted. 1.1.1 The 3-hour Interplanetary K Index shall be estimated in Kp units. FR 1.1.1-1 The 3-hour Interplanetary K Index shall be estimated with an update interval of less than or equal to 3 hours. PR 1.1.1-2 The 3-hour Interplanetary K Index shall be estimated with a latency of less than or equal to 5 minutes. Geomagnetic storms shall be determined at Space Weather Scale levels G1 through G5. 1.1.2 N/A N/A PR FR 1.1.2-1 An alert observation shall be generated when any geomagnetic storm Space Weather Scale value is reached. PR 1.1.2-2 A forecast duration shall be generated when a geomagnetic storm alert observation is provided. PR 1.1.2-3 An event summary message for a prior alert observation shall be generated when the geomagnetic storm Space Weather Scale value decreases below the alert value. Space weather alert observations shall be generated for geomagnetic storms with a latency of less than or equal to 1 minute 1.1.2-4 N/A 2.1.1 Geomagnetic storms shall be forecasted at Space Weather Scale levels G1 through G5. N/A N/A N/A PR PR 1.2 Solar radiation storms shall be observed. FR 1.2.1 Solar proton flux shall be measured in particle flux units. FR 1.2.1-1 Solar proton flux, from 10-² particle flux units to 10⁶ particle flux units, shall be measured with an accuracy of plus or minus 25 percent. PR 1.2.1-2 Five-minute integrated proton flux shall be measured for particles greater than or equal to 10 megaelectronvolts. PR 1.2.1-3 Five-minute integrated proton flux shall be measured for particles greater than or equal to 100 megaelectronvolts. PR 1.2.1-4 Solar proton flux shall be measured with a sampling interval of less than or equal to 10 minutes. PR 2.1.1-1 Forecasts for geomagnetic storms shall be generated with a latency of less than or equal to 15 minutes. 2.2 Solar radiation storms shall be forecasted. N/A N/A N/A N/A N/A C-18 1.2.1-5 1.2.2 Solar proton flux shall be measured with a latency of less than or equal to 1 minute. Solar radiation storms shall be determined at Space Weather Scale levels R1 through R5. FR 1.2.2-1 An alert observation shall be generated when any solar radiation storm Space Weather Scale value is reached. PR 1.2.2-2 A forecast duration shall be generated when a solar radiation storm alert observation is provided. PR 1.2.2-3 An event summary message shall be generated for a prior alert observation when the solar radiation storm Space Weather Scale value decreases below the alert value. Space weather alerts (observations) shall be generated for solar radiation storms with a latency of less than or equal to1 minute. 1.2.2-4 2.2.1 Solar radiation storms shall be forecasted at Space Weather Scale levels R1 through R5. N/A N/A N/A PR PR 1.3 Galactic cosmic rays shall be observed in megaelectronvolts. FR 1.3-1 Galactic cosmic rays shall be observed from 100 megaelectronvolts to 2,000 megaelectronvolts with an accuracy of 5 percent. PR 1.3-2 N/A PR An alert observation shall be provided when galactic cosmic rays greater than or equal to 100 megaelectronvolts are observed when greater than 10 percent above median background. PR 1.3-3 A forecast duration shall be provided when a galactic cosmic ray alert observation is provided. PR 1.3-4 An event summary message for a prior alert observation shall be provided when galactic cosmic rays decrease below 10 percent above median background. PR 1.3.5 Space weather alerts (observations) for galactic cosmic rays shall be provided with a latency of less than or equal to1 minute. PR 1.4 Solar flares shall be observed. FR 1.4.1 Solar X-Ray flux shall be measured in Watts per meter squared. FR 1.4.1-1 Solar X-Ray flux shall be measured in the 1-8 Angstrom passband. PR 1.4.1-2 Solar X-Ray flux shall be generated in 5 minute averages. PR 1.4.1-3 Solar X-Ray flux shall be generated with an update interval of less or equal to 5 minutes. PR 2.2.1-1 Solar radiation storms shall be forecasted with a latency of less than or equal to 15 minutes. 2.3 Galactic cosmic rays shall be forecasted in megaelectronvolts. 2.3-1 Galactic cosmic rays from 100 megaelectronvolts to 2,000 megaelectronvolts shall be forecast when greater than 10 percent above median background. N/A N/A N/A 2.3-2 Forecasts for galactic cosmic rays shall be provided with a latency of less than or equal to 15 minutes. 2.4 Solar flares shall be forecasted. C-19 1.4.1-4 Solar X-Ray flux shall be measured with an accuracy of plus or minus 10 percent. 1.4.1-5 Solar X-Ray flux shall be provided with a latency of less than or equal to 5 minutes. Radio blackouts shall be determined at Space Weather Scale levels R1 through R5. 1.4.2 PR PR FR 2.4.1 Radio blackouts shall be forecast at Space Weather Scale levels R1 through R5. 1.4.2-1 An alert observation shall be generated when any radio blackout Space Weather Scale value is reached. PR N/A 1.4.2-2 A forecast duration shall be generated when a radio blackout alert observation is provided. PR 1.4.2-3 An event summary message for a prior alert observation shall be generated when the radio blackout Space Weather Scale value decreases below the alert value. PR 1.4.2-4 Space weather alerts (observations) for radio blackouts shall be provided with a latency of less than or equal to 1 minute. PR 1.5 The auroral boundary shall be observed. FR N/A 1.5.1 Power flux shall be measured in gigawatts. FR N/A 1.5.1-1 An auroral activity estimate for greater than 30 degrees north and south latitude shall be generated with a horizontal resolution of 50 kilometers. PR 1.5.1-2 An auroral activity estimate shall be generated with a measurement accuracy of plus or minus 50 kilometers. PR 1.5.1-3 An auroral activity estimate shall be generated with a update rate of less than or equal to 90 minutes. PR 1.5.1-4 An auroral activity estimate shall be provided with a latency of less than or equal to 15 minutes. PR 1.6 Ionospheric activity shall be observed. FR 1.6.1 Total electron content shall be measured in total electron content units. FR 1.6.1-1 Total electron content shall be measured with a horizontal resolution of 100 kilometers. PR N/A N/A 2.4.1-1 Radio blackout Space Weather Scale Values shall be forecasted with a latency of less than or equal to 15 minutes. N/A N/A N/A N/A N/A N/A N/A C-20 1.6.1-2 Total electron content shall be measured from 0 to 400 total electron content units with an accuracy of plus or minus 6 total electron content units. PR 1.6.1-3 Total electron content shall be generated with an update interval of less than or equal to 15 minutes. PR 1.6.1-4 Total electron content shall be provided with a latency of less than or equal to 15 minutes. PR 1.7 D-region absorption prediction product shall be generated. FR 1.7-1 D-region absorption prediction product shall be generated with a horizontal resolution of 5 degrees latitude and 15 degrees longitude. PR 1.7-2 D-region absorption prediction product shall be generated with an update interval of less than or equal to 5 minutes. PR 1.7-3 D-region absorption prediction product shall be provided with a latency of less than or equal to 1 minute. PR N/A FR 2.5 Space weather forecasts shall be provided. N/A PR 2.5-1 A 7-day space weather outlook forecast shall be provided once per day. N/A PR 2.5-2 A 3-day space weather forecast shall be provided once per day. 2.5-3 A 30-hour space weather forecast shall be provided less than or equal to every 6 hours. 2.5-4 The 30-hour space weather forecast shall be amended when the observed Space Weather Scale level varies from the forecast level. 2.5-5 The 30-hour space weather forecast shall be amended when the forecast timing for an event changes by greater than or equal to one hour within 6 hours. 2.5-6 The 30-hour space weather forecast shall be amended when a previously non-forecast space weather event is expected within 6 hours. The 30-hour space weather forecast shall be amended when the current forecast Space Weather Scale value needs to be changed to a different level within 6 hours. N/A N/A N/A PR PR N/A N/A N/A N/A N/A N/A N/A PR N/A PR N/A 2.5-7 PR N/A N/A FR 2.6 2.6-1 PR C-21 Space weather forecasts shall be verified (confidence level). Space weather forecasts shall be verified, for forecast period(s) from 0 to less than or equal to 6 hours, with an accuracy of greater than or equal to 75 percent by 2016. N/A 2.6-2 PR N/A 2.6-3 PR N/A 2.6-4 PR N/A 2.6-5 PR N/A 2.6-6 PR N/A 2.6-7 PR N/A 2.6-8 PR N/A 2.6-9 PR N/A 2.6-10 PR N/A 2.6-11 PR N/A 2.6-12 PR C-22 Space weather forecasts shall be verified, for forecast period(s) from 0 to less than or equal to 6 hours, with an accuracy of greater than or equal to 95 percent by 2025. Space weather forecasts shall be verified, for forecast period(s) from greater than 6 hours to less than or equal to 30 hours, with an accuracy of greater than or equal to 65 percent by 2016. Space weather forecasts shall be verified, for forecast period(s) from greater than 6 hours to less than or equal to 30 hours, with an accuracy of greater than or equal to 85 percent by 2025. Space weather forecasts shall be verified, for forecast period(s) from greater than 30 hours to less than or equal to 3 days, with an accuracy of greater than or equal to 55 percent by 2016. Space weather forecasts shall be verified, for forecast period(s) from greater than 30 hours to less than or equal to 3 days, with an accuracy of greater than or equal to 75 percent by 2025. Space weather forecasts shall be verified, for forecast period(s) from greater than 3 days to less than or equal to 7 days, with an accuracy of greater than or equal to 45 percent by 2016. Space weather forecasts shall be verified, for forecast period(s) from greater than 3 days to less than or equal to 7 days, with an accuracy of greater than or equal to 75 percent by 2025. Space weather forecasts shall be verified, for forecast period(s) from 0 to less than or equal to 12 hours, with a timing accuracy of plus or minus 1 hour. Space weather forecasts shall be verified, for forecast period(s) from greater than 12 hours to less than or equal to 30 hours, with a timing accuracy of plus or minus 3 hours. Space weather forecasts shall be verified, for forecast period(s) from greater than 30 hours to less than or equal to 3 days, with a timing accuracy of plus or minus 6 hours. Space weather forecasts shall be verified, for forecast period(s) from greater than 3 days to less than or equal to 7 days, with a timing accuracy of plus or minus 12 hours. Note: This PR will not be required if an outlook will be verified by occurrence anytime within the 3 to 7 day period with no timing accuracy requirements. If a 12 hr timing accuracy is desired, this PR will apply. APPENDIX D: SPACE WEATHER IMPACTS ON AVIATION Communications – Polar Cap Absorption Impact A Polar Cap Absorption (PCA) event results from the ionization of the D-layer of the polar ionosphere by SEPs - high energy protons (see #5 under Section 4.3.1 for details). A PCA causes a HF radio blackout for trans-polar circuits and can last up to several days. PCAs are almost always preceded by a major solar flare with the time between the flare event and the onset of the PCA ranging a few minutes to several hours. Consequently, air traffic cannot operate over the polar cap during these conditions. Radio blackouts: disturbances of the ionosphere caused by X-ray emissions from the Sun. HF radio degradation or blackouts are possible. Radio blackouts primarily affect HF communication frequencies (3-30MHz) although detrimental effects may spill over to VHF (30-300MHz) and beyond in fading and diminished ability for reception. The blackouts are a consequence of enhanced electron densities caused by the emissions from solar flares that ionize the sunlit side of the Earth. The duration of dayside solar flare radio blackouts closely follows the duration of the solar flares that cause them beginning with the arrival of the X-ray and EUV photons, and abate with their diminution. Usually the radio blackouts last for several minutes, but they can last for hours. There is also a class of longer duration radio blackouts that occur in the polar and very highlatitude regions that are a result of entirely different physics and have characteristics very much different from the radio blackouts in equatorial and mid-latitudes, caused by solar flares. These polar radio blackouts will be described in the Solar Radiation Storm section of this appendix. Satellite-based navigation, though most affected near the poles and the equator, can be impacted at middle latitudes. The solar activity on GPS that occurred in December 2006 when a solar radio burst in a solar flare was so strong that it overwhelmed the GPS signal at L-band, causing a several-minute-long interruption to geodetic-grade GPS receivers operating on the dayside of Earth. Notwithstanding rules for controlled flights from ICAO Annex 2 and 11, which state that aviation communications are either possible according to paragraph 3.6.5, or the ICAO communication failure rule have to be followed:27 An aircraft operated as a controlled flight shall maintain continuous air-ground voice communications watch on the appropriate communication channel of, and established two-way communication as necessary with, the appropriate Air Traffic System (ATS) authority in respect of aircraft forming part of aerodome traffic at a controlled aerodome. 27 Annex 11, Chapter 6, Air Traffic Services Requirements for Communications, para 6.1.2.2 D-1 Note 1: Selective Calling (SELCAL) or similar automatic signaling devices satisfy the requirement to maintain an air-ground voice communication watch. Note 2: The requirement for an aircraft to maintain an air-ground communication watch remains in effect after CPDLC has been established. Consideration for future improvements may include definition of dimensions for affected areas for trans-oceanic communications, on the sunlit side of the Earth. Radiation – Communication and Human Impacts The issue of unhealthy radiation exposure on humans was brought to light when polar flight routes were opened over the last decade. This document purposely does not go into detail defining requirements of capabilities/functions to be included on radiation effects on humans. This challenge will be handled by individual entities within their respective operations for the near-future with reference to the safety Management Systems concept and ICAO handbook 9859 as well as the ICRP guidance on radiological protection. Commercial aviation routine flights at polar high latitudes operate in an environment that has the least protection from the Earth’s atmosphere from highly charged ionized particles due to the configuration of the magnetic field lines. Consideration of future improvements need to address communication HF outages over the polar region. Current practice in the southern hemisphere excludes the entire polar region for each event. But there were measurements made at higher flight altitudes over the Great Lakes at lower latitudes that measured increased radiation exposure to warrant concern during the Halloween 2003 solar storm event. The increased dosage in radiation also depends on the spectrum of the solar radiation storm. The more intense the solar storm, the higher the energies of the proton particles, the so-called “hard” spectrum, at the top of the atmosphere, causing radiation dose increases that raise concern for human health. The measurements from aircraft on high latitude routes have shown real increases in the radiation dose rate during solar radiation storms. On April 15, 2001 a radiation storm with a hard spectrum occurred as a commercial airline flight from Frankfurt to Dallas – Fort Worth carrying dosimeters caught the onset, peak, and decay of the radiation increase during flight. SWx data from the Moscow Neutron Monitor confirmed the solar eruption. The finding was the radiation dose increased by a factor 2 to 2.5 before returning to near background levels after approximately three hours. This is but one example of data taken from aircraft showing the increased dose rate during solar radiation storms.28 28 NOAA, Space Weather Prediction Center (SWPC), Manual on Space Weather Effects in Regard to International Air Navigation (January 2011). D-2 Solar Radiation Storms: elevated levels of radiation that occur when the numbers of and the energy levels of SEP increase. Typical effects from solar radiation storms include degradation to satellite sensors, memory micro-chips, and power systems, radiation hazards to humans in flight at high altitudes and/or high latitudes. HF radio blackouts and induced positional errors to GPS are also possible. Solar radiation storms occur when large quantities of charged particles, primarily protons, are accelerated by processes at or near the Sun and then the near-Earth environment is bathed with these charged particles. These particles cause an increase in the radiation dose to humans, and create an increased possibility of single event upsets in electronics. Earth’s magnetic field and atmosphere offer some protection from this radiation, but that shielding decreases with altitude, latitude, and magnetic field strength and direction. The polar region on Earth are most vulnerable to these charged particles, because the magnetic field lines at the poles extend vertically downwards intersecting Earth’s surface, which allows the particles to spiral down the field lines and penetrate into the atmosphere increasing the ionization. A significant factor relating to the criticality of the radiation increase at Earth is the spectrum – the energy distribution – of the solar protons. Earth will be bathed by protons of varying energies, as a function of the eruption at the Sun and the magnetic connection between the Sun and Earth. High-energy protons, the so-called “hard” spectrum, cause radiation dose increases that are of concern to human beings. Lower energy protons, the “soft” spectrum, have little effect on humans but have a severe impact on the polar ionosphere and high latitude HF propagation. The duration of solar radiation storms is affected by the magnitude of the solar eruption as well as the received spectrum. For events that are of a large magnitude but a soft spectrum, the duration may last for one week. Events that are of large magnitude but a hard spectrum may last for only a few hours. There is a great diversity in the duration of solar radiation storms, as there are many factors that contribute to the acceleration and propagation of the charged particles near Earth. Some definition of contingency procedures should be considered for example descent to lower altitude for all aircraft from safety of flight prospective. But additional consideration should be given to applying updated provisions of the ICAO document 4444 governing the descent of any futuristic routinely flying air vehicle being forced in unscheduled manner to descent into altitudes with of traffic capacity due to solar radiation over those portions of the airspace, where non-forecasted effects of solar events are now expected.29 These solar radiation storm effects could be displayed in graphical text service product described in the FAA handbook on the Solar Radiation Alert System below: 29 Document 4444, Chapter 15, paragraph 15.5.4, for Descents due to Solar Cosmic Radiation D-3 Solar Radiation Alert System (Revised 30 May 2008) DOT/FAA/AM-09/6, Office of Aerospace Medicine Washington, DC 20591 This document does not go into any detail on existing general rules describing human exposure to ionizing radiation. The generally accepted principle of radiation protection being the ALARA principle (As Low As Reasonably Achievable – taking into account economic and social considerations), detailed rules are laid down in documents such as: ICRP 103, International Commission on Radiological Protection, Publication 103, 2007 Recommendations of the International Commission on Radiological Protection with an annual limit of 20 mSv for occupational exposure for airline flight crews and, NEA Paper 6920 ICRP Recommendations/ EU BSS Draft 24.02.2010 according to which, for example, the recognition of flight personnel as Category A occupationally exposed workers is necessary, as they are liable to receive an effective dose D-4 greater than 6 mSv per year. Flight personnel with an effective dose of more than 1mSv/yr should be recognized as occupationally exposed to ionizing radiation.30 30 Office of Aerospace Medicine, Washington, DC, DOT/FAA/AM-03/16 (October 2003). D-5 Navigation - Avionic Error Impacts Resulting from Solar Activity Aircraft en route poleward of 780N and 600S of latitude can experience large errors in tracking aircraft position during a disruptive SWx event. The electronic components of aircraft avionic systems are susceptible to damage from the highly ionizing interactions of cosmic rays, solar particles and the secondary particles generated in the atmosphere. As the size of these component chips become smaller, and therefore more susceptible to SWx, the risk of highly charged particles from SWx activity corrupting micro-chips increases and can lead to erroneous outputs during flight operations. These software errors are referred to as Single Event Upsets (SEU). This problem is expected to increase as more, low-power, small feature size electronics are deployed in “more electronically enabled” aircraft, which usually do not have redundant systems. Data collected from satellites incorporating sensitive Random Access Memory (RAM) chips have had upset rates from one per day without solar activity to several hundred per day during solar radiation storm.31 Geomagnetic Storms: disturbances in the geomagnetic field caused by gusts in the solar wind that blows by Earth. Typical effects from geomagnetic storms include degradation of HF radio transmissions, satellite navigation degradation, and disruption of low frequency radio navigation systems. Geomagnetic storms can also disrupt ATC facilities and other national airspace components are susceptible to these power outages. The duration of geomagnetic storms is usually on the order of days. The strongest storms may persist for almost one week, and a string of CMEs may cause prolonged disturbed periods related to the additional energy being pumped into the system. The intensity of geomagnetic storms is often given in terms of the K index. In general terms, the K index captures the variance from the quiet day behavior of the geomagnetic field, and is measured every three hours. The K index ranges from 0 (most quiet) to 9 (most disturbed). More detailed description of the indices is given later in this section. The NOAA G-Scales describe the most intense storms, the extreme G5 level events, as having at least one K = 9 occurring, the highest K index attainable. A NOAA G-Scale minor (G1) K = 5 storm is thought to be the level of disturbance with the least noticeable impact.32 31 American Meteorological Society (AMS) and SolarMetrics, Policy Workshop Report, Integrating Space Weather Observations and Forecasts into Aviation Operations (March 2007), www.ametsoc.org/atmospolicy 32 NOAA, Space Weather Prediction Center (SWPC), Manual on Space Weather Effects in Regard to International Air Navigation (January 2011). D-6 Figure 8: The Time Scales of Solar Effects (Source: NOAA SWPC) Eight minutes after a flare and/or a CME erupts from the Sun, the first blast of EUV and X-ray light increases the ionospheric density, which can impact HF communication loss. D-7 APPENDIX E: SPACE WEATHER ALERT AND FORECAST PRODUCTS SWx alerts and warnings need to be integrated into the normal operations of commercial airlines on a more frequent basis. SWx alerts are issued for these categories. Alerting criteria and descriptions for the SWx activities below would be provided in concert with the NOAA Space Weather Scales presented in the Table 1, Table 2, and Table 3.33 33 X-ray Flux Alert and Event Summaries Radio Burst Alerts and Summary Geomagnetic Sudden Impulse Warning and Alert Geomagnetic K-index Warnings and Alerts Geomagnetic A-index Watches Electron Flux Alert Proton 10MeV and 100MeV Flux Warnings, Event Alerts and Summaries SWPC website: www.swpc.noaa.gov (Alert/Warnings) E-1 NOAA’s SWPC is currently providing SWx alerts and forecasts and information to the user as follows:34 Alerts and Forecasts Title Info Update Latest Older SWPC Space Weather Alerts; watches, warnings, alerts, and summaries Info when issued latest Sept 2001 Space Weather Advisory Bulletin Info when issued latest 6 months 3-hourly WWV Geophysical Alert Message Info 3 hours latest 75 days Solar and Geophysical Activity Report and 3day Forecast Info 2200 UT web, ftp file last 75 or warehouse 3-day Space Weather Predictions Info 2200 UT latest 75 days 45-day Ap and 10.7cm Forecast -- 2114 UT latest 20 days Weekly Highlights and 27-day Forecast Info Tuesday latest 1997 27-day 10cm, Ap, and Max Kp Outlook Info Tuesday latest 1997 Space Weather Advisory Outlook Info Tuesday latest 6 months Solar Cycle Progression Info Monthly web ftp ssn -flux -- Predicted Monthly Sunspot Number & 10cm Radio Flux Info Monthly latest -- As Conditions Warrant Daily or less Weekly Monthly 34 SWPC website: www.swpc.noaa.gov (Alert/Warnings) E-2 Current Support Environment Collective international efforts have resulted in the availability of SWx advisory products displays, forecasts, and warning messages from the NOAA SWPC operationally supported 24 hours a day, seven days a week.35 SWPC Reports and Summaries Title Info Update Latest Older Archive Info 5 min updating no no -- 5 min updating no no SW for Aviation Service Providers Info 1 min updating no no Solar and Geophysical Activity Report and 3-day Forecast Info 2200 UT web, ftp file 75 days 1996 Solar Region Summary Info 0030 UT latest 75 days 1996 Solar and Geophysical Activity Summary Info 0245 UT latest 75 days 1996 Daily Summary of Space Weather Observations Info 0200 UT latest 75 days no GEOALERT Info 0330 UT latest 75 days 1996 Weekly Highlights and 27-day Forecast Info Tuesday latest 1997 SWPC "The Weekly" - Preliminary Report and Forecast of Solar Geophysical Data Info Tuesday latest 1997 SWPC Info monthly latest cycle no Daily or less "Space Weather Now" "Today's Space Weather" Weekly Monthly Solar Cycle Progression Longer Solar Proton Events Affecting the Earth Environment SWPC Forecast Verification -- as needed 2005 1976 SWPC Info yearly 2003 1986 SWPC This ConOps will convey how SWx alerts and warnings can be integrated into DSTs. 35 SWPC website: www.swpc.noaa.gov (Alert/Warnings) E-3 APPENDIX F: DELINEATING REGIONS OF SPACE WEATHER IMPACT The geomagnetic field is a continuum and therefore different SWx phenomena affect geomagnetic latitudes in various ways. The geomagnetic science arena has delineated such with regard to their geographic distribution of modern ground-based ionosphere observatories around the world. Part of the effort for global harmonization of SWx information in a single standard is to encapsulate the intensity and expected impacts in a temporal and spatial sense. This geomagnetic geographic latitude stratification may help frame a watch/warning/alert/update type message for the aviation industry to better interpret and picture the solar event in flight planning or tactical maneuvers while en route. Perhaps SWx effects on global airspace could be delineated along these boundaries already established as depicted in Figure 9.36 Depending on the type and severity of the solar event, its impact can vary over different magnetic latitudes and be captured in a more understandable display from a visual prospective of the user. The variety of users who can better grasp the magnitude of the expected impact at the different magnetic latitudes along the long-haul route would certainly help in the flight planning in various ways to mitigate the lost in operational efficiency and cost. 36 Dr. Jeffrey J Love, USGS, 8th Conference on Space Weather, 91st Annual AMS Conference, Long-Term Change in Geomagnetic Activity Presentation (January 2011). F-1 Figure 9: Magnetic Latitudes Already Established for Magnetic Observatories Around the World Note: The Auroral Electrojet does exist in the southern hemisphere but is not measured due to the total lack of monitoring stations (notice no orange color dots similar to the northern hemisphere) because of the absence of land areas to establish the necessary monitoring network F-2 APPENDIX G: BI-LATERAL AGREEMENTS The Federal Aviation Administration (FAA) will work with European Aviation Safety Agency (EASA) as the authority representing those European Union Member States and EASA associated countries with who the U.S. currently has existing bi-lateral agreements. Additionally, FAA Order 8100.14 describes the continuing working relationship between the FAA and EASA. There was an international executive agreement and its two annexes (Airworthiness and Maintenance) to the overall agreement signed on June 30, 2008. However, the new agreement will not enter into force until resolution of pending Congressional legislative language regarding inspection of foreign repair stations. FAA approval of European products, parts, and appliances will continue for those products covered under a bilateral agreement with an European Union Member State. Until a new bilateral agreement is concluded with the Community that would govern the acceptance of products between the U.S. and the entire Community as a single entity, the FAA can only accept applications for validation and import into the US of products, parts and appliances from European Union Member States within the scope of the current bilateral agreements G-1 APPENDIX H: INTRODUCTION TO SPACE WEATHER Space weather (SWx) can be defined as the conditions on the Sun and in the solar wind, magnetosphere, ionosphere, and thermosphere that can influence the performance and reliability of space-borne and ground-based technological systems and can endanger human life or health of aviation flight crews and passengers.37 Unlike terrestrial weather, SWx effects can be global with the onset of their impacts on the earth’s atmosphere. The time-scale comparison of impacts on aviation altitudes is also much more rapid following the eruptive episode from either the Sun’s surface and/or solar outer atmosphere. These events can occur independently or together. Solar flares are the eruptions from the Sun’s surface and a CME is an eruption of a large volume of the Sun’s atmosphere – the Corona. These magnetic energy events interact with the Earth’s magnetosphere, which allows the highly charged particles from the Sun to travel along the magnetic field that converges at the poles and penetrate into lower altitudes – aviation altitudes. Ground-based instruments and space-based sensors measure the magnetic fields of highly charged particles emitted from the Sun to help better understand and predict potential impacts from SWx activities. The electronic components of aircraft avionic systems are susceptible to damage or interference from the highly ionizing interactions associated with cosmic rays, solar particles and the secondary particles generated within the Earth’s atmosphere. Electromagnetic energy associated with a single solar storm on the Sun’s surface is projected out into deep space traveling at the speed of light, arriving at the Earth in about eight minutes. The transit time for energetic particles associated with a CME from the Sun for the same solar event takes longer to reach the Earth’s atmosphere, from tens of minutes to a few hours, depending on the characteristics and source locations of the emitted particles. Since the Sun is a variable star, its output can vary over a wide range of time-scales depending on the type of solar event (solar flares, solar protons from Radiation Storms), as well as over the long-term eleven-year solar cycle, with Extreme Ultra Violet (EUV) radiation, for example, dimming and brightening by a factor of four or five. 37 WMO Space Programme SP-5, The Potential Role of WMO in Space Weather (April 2008). H-1