Summary of the JWST Integrated Science Instrument Module (ISIM) and Structural/Thermal Subsystem Systems Requirements Reviews (SRRs) Jerry Kriss 04/15/2004 TIPS/JIM 1/13 ISIM Overview ISIM is: • The JWST Science Instruments • Associated Infrastructure: Structure, C&DH, & FSW Region 1 Science Instrument Optics Assemblies Near Infrared Camera (NIRCam) Near Infrared Spectrometer (NIRSpec) Mid Infrared Instrument (MIRI), & Dewar Fine Guidance Sensor and Tunable Filter (FGS/TF) Optical Bench Structure Radiators and support structure (NGST supplied) Region 2 Focal Plane Electronics (FPE) Instrument Control Electronics (ICE, MCE, DCE) Region 3 ISIM Command & Data Handling (C&DH) Electronics FGS C&DH Electronics 04/15/2004 TIPS/JIM 2/13 JWST System Constituents System JWST System Segment Observatory Ground Launch Element Optical Telescope Element (OTE) Science and Operations Center Launch Vehicle Spacecraft (SC) Institutional Systems Payload Adapter Integrated Science Instrument Module (ISIM) Common Systems Launch Site Services NIRCam Subsystem (within ISIM) Structure 04/15/2004 NIRSpec MIRI FGS/TF Thermal IC&DH Flight SW TIPS/JIM Harnessing 3/13 JWST Requirements Tree Baselined In CM Review Drafts Available Allocation Documents JWST Program Plan JWST-PLAN-000633 L1 Program System FGS SRD JWST Science Requirements Document JWST-RQMT-002558SR NIRCam SRD NIRSpec SRD JWST Mission Requirements JWST-RQMT-000634 MR JWST Performance Assurance Requirements JWST-RQMT-000650 PA JWST Mission Operations Concept Document JWST-OPS-002018 MOC FGS OCD MIRI SRD Budgets WFE Rev Q 03-JWST-0405 Efficiency Pointing WFS&C Requirements Allocation Document JWST-RQMT-002017 WFS NIRCam OCD EMC Control Plan JWST-PLAN-002449 NIRSpec OCD EMC Performance Quality Assurance Plan JWST-PLAN-002412 Contamination Control Plan JWST-PLAN-002028 CCP PQ MIRI OCD Segment Flight Observatory to Ground Segment IRD JWST-IRD-000696 FG Ground Segment Requirements JWST-RQMT-001056 GS JWST Observatory Specification JWST-SPEC-002020 RD Launch Segment Specification JWST-SPEC-001999 OL OBS JWST-ICD-001998 FGC Radiation Requirements Allocation Specification JWST-SPEC-000871 Observatory to Launch Segment IRD JWST-IRD-002000 JWST System Verification Plan JWST-PLAN-002027 LS JWST-ICD-002001 OLC Environmental Req’s for the JWST Observatory JWST-SPEC-003149 EV Observatory I&T Plan JWST-PLAN-002030 Observatory to GSE IRD D36127 OG D36128 OGC Fault Protection Requirements Document JWST-RQMT-002450 FP Element ISIM Requirements Document JWST-RQMT-000835 ISIM ISIM to OTE and Spacecraft IRD JWST-IRD-000640 ISIM to OTE and IOS-IR JWST-ICD-001831 04/15/2004 SC Requirements Document JWST-RQMT-002039 SC Spacecraft to OTE ICD D35231 SOIC OTE Specification JWST-RQMT-002021 OTE IOSC TIPS/JIM 4/13 ISIM SRR Objectives Confirm that ISIM-level requirements meet the mission objectives. Validate that the ISIM architecture concept can support the functional, operational, interface and performance requirements. Confirm that the preliminary system design is ready to proceed. 04/15/2004 TIPS/JIM 5/13 Requirements Traceability •L1-1 Density of Galaxies, L1-2 Spectra of Galaxies •SR-4 Diffraction-Limited imaging 2.0 mm-27 mm, SR-5 Short-l image quality: ~75% @ 150 mas @ 1 mm, SR-21 Sensitivity MRD Appendix A MR-51 SNR equations, conditions, and assumptions The observatory system shall be capable of reaching the sensitivity performance levels shown in the following table when observing a position on the celestial sphere that exhibits 1.2 times the minimum Zodiacal light background power. Current draft: JWST-MEMO-002852 JWST-TM-002876 JWST-TM-002877 JWST-TM-002878 Sensitivity KEY OTE/SC REQUIREMENTS Transmission: MR-211 Image quality: MR-110,111,228 Stray light: MR-121,122 Collecting area: MR-198 Observatory Specification: OBS-67 Allocation ISIM Requirements Sec 3.7.1 ISIM Requirements Section 3.2 ISIM Requirements Sec 3.7.2 ISIM Requirements Sec 3.7.3 ISIM Requirements Sec 3.7.4 NIRCam FRD NIRSpec FRD MIRI FRD FGS-TF IPFRD Derived sensitivity for each operating mode Derived sensitivity for each operating mode Derived sensitivity for each operating mode Derived sensitivity for each operating mode 20% allocated margin 20% allocated margin 20% allocated margin 20% allocated margin 04/15/2004 TIPS/JIM 6/13 Open Trade Studies Pupil Imaging Lens in NIRCam • Concluded in favor of including a pupil imaging lens. OTE/ISIM Mechanical Interface • Concluded in favor of mounting the ISIM to the OTE BSF. ISIM Decontamination • Concluded in favor of preventing contamination by managing cooldown. Reheating ISIM and instruments rejected as an option. MIRI Dewar • Baseline is dual solid hydrogen dewar w/ tactical cooler on the pad. • To be concluded after dewar contractor selected. ISIM Electronics Compartment (IEC) Accommodation • Outstanding mass and thermal problems. TBD by 8/2004. OTE Simulator (OSIM) • To be concluded by mid-summer 04/15/2004 TIPS/JIM 7/13 Key Issues & Challenges MIRI SRR • Delta-SRR successfully accomplished 9 March 2004 • Demonstrated proper Requirements flowdown • Answered all RFAs Instrument Electronics Accommodations Trade • Lacking Observatory architectural solution to housing ISIM electronics that meets all thermal, structural, and electrical performance requirements • Trade study underway to develop new concept for electronics compartment • Goal to keep all Instrument electronics boxes in Region 2 • Planned completion date July 04 System Mass • Observatory Mass Budget has only 9% unallocated reserve • Estimates currently exceed allocations • ISIM allocation includes growth contingency • Tracking SIs and Subsystem mass estimates and contingency usage monthly • Mass evaluation and reallocation (if necessary) in September following: • Conclusion of IEC Trade Study • Conceptual Design of MIRI Dewar 04/15/2004 TIPS/JIM 8/13 Work In Progress Sensitivity • Mission Rqmts Document and Observatory Spec update required to reflect current OTE and Instrument designs. Focus and Pupil Shear Budgets • Tentative agreement; CCRs to Interface Rqmts Docs in process. Accommodation of NIRCam non-common-path Wavefront Error • Methodology defined; CCRs to Instrument Interface Rqmts Docs in process Coronagraphy • Existing Level 1 Requirement for Coronagraphy to be flowed to lower level requirements documents (Mission -> Observatory -> ISIM) • NIRCam, MIRI, and FGS/TF concepts already include coronagraphy Stray Light and Thermal Emissions Budget • Working group defining format and allocations for flowdown of Mission-level requirement 04/15/2004 TIPS/JIM 9/13 Plans to ISIM SDR Complete Trade Studies Key Procurements • Select NIRSpec Contractor Team • Select MIRI Dewar Manufacturer • Select Structure Manufacturer • Select Single Board Computer Supplier Documentation • Complete CCB Process for: • ISIM, SI, and ISIM Subsystems Requirements Documents • Flight and ETU ISIM Integration and Test Plans • MIRI, NIRSpec, FGS Joint Project Implementation Plans • Develop drafts of: • SI Interface Control Documents Achieve TRL6 for Detector Technologies Complete Instrument and Subsystem SRRs and PDRs 04/15/2004 TIPS/JIM 10/13 ISIM SRR Summary Results The board thought that the review was excellent. 23 Requests for Action (RFAs) generated. Major issues raised by the review board: • ISIM urged to speed up I&T timeline to meet up with OTE Pathfinder at Plumbrook. • Worried about piecemeal approach to contamination control. • Worried that redundancy and cross strapping is being done to excess, without careful thought. • The connection with Ariane Space is still missing, and it can affect many requirements. • Desire to make several of the ISIM FSW rqmnts less vague and more verifiable. • Need to do a better flow down of the efficiency rqmt and tie it in to data quality and reliability in a more comprehensive way. • Fault handling requires more development. 04/15/2004 TIPS/JIM 11/13 Structural/Thermal Subsystem SRR Structure • Provides kinematic interface to Optical Telescope Element • Supports Instrument Optical Assemblies and maintains alignment • Composite carbon-fiber (M55J) construction with metal (Ti) fittings Structural system risks: • Thermal distortion at cryogenic temperatures. • Mitigation: Math Model Development plus test program. • Metal-composite joint survivability. • Mitigation: early and extensive test program. Thermal Control Subsystem • Maintains thermal environments for instruments, structure, and electronics • Heat Straps, Thermal Switches, MLI, Heaters, & Sensors • Heat straps connect to radiators for passive cooling (radiators are NGST-provided) • MIRI dewar is provided by MIRI/JPL Thermal system risks: • Managing cool down so that it is rapid enough to enable commissioning within the first 6 months. • Managing relative thermal profiles to avoid contamination. 04/15/2004 TIPS/JIM 12/13 Structural/Thermal SRR Summary Review was successful. ~20 RFAs generated. Major concern of the panel: • Little/no flight history for cryogenic applications of composite structures, especially composite joints. • Urged an even more aggressive and earlier testing program than described by the team. 04/15/2004 TIPS/JIM 13/13