Critical Design Review 02/02/ 2012 Project Phoenix 2011-2012 The Pennsylvania State University 1 Presenters • • • • • • • • • • • Russell Moore – Project Manager Brian Taylor – Systems Engineer Matt Hanna – Structures & Aerodynamics Lead Tony Maurer – Structures & Aerodynamics Lead Heather Dawe – Propulsion Lead Rob Algazi – Propulsion Lead Adam Covino – Payload Lead Brian Lani – Payload Lead Eric Gilligan – Avionics & Recovery Lead Lawrence Digirolamo – Avionics & Recovery Lead Tom Letarte – Safety Officer 2 Discussion Topics • • • • • • • • Overview Structures & Aerodynamics Avionics & Recovery Propulsion Payload Safety and Quality Assurance Outreach Conclusion 3 Overview (Project/Vehicle) • Rocket is 92.2” in length, 4.5” in diameter (OD)- 4.375” (ID)and weighs 29 lbs. • Uses machined fin brackets, motor retainer and tail cone. • Recovery System is Single Ejection (CO2)/Dual Deployment 4 Fin Bracket • Allows for easy replacement of damaged fins • Allows experimentation of fin design (to alter the CP and therefore Static Stability) • CNC machined aluminum – No epoxy or other permanent bond • Screws into fin and through body tube 5 Motor Retainer • Machined Aluminum forward motor retainer • Attaches to motor casing • Screwed into airframe – No epoxy or other permanent bonds • Acts as an Av bay aft bulk plate 6 Tail Cone • CNC machined aluminum aft motor retainer • Reduces drag up to 50% for subsonic flight [1] • Threads onto aft of booster section – No epoxy or other permanent bonds • Opens up more room in airframe 7 Structures • Rocket Flight Static Stability – 1.4 3000 2500 Predicted Drift (ft) • Current Simulated Mass: 29.3 pounds • Mass Margin: 2.6 pounds • Predicted Drift 2425 2000 1500 1480 1000 930 500 425 0 0 5 10 15 20 25 Wind Speed (mph) Predicted drift as a function of wind speed for the current mass estimate (483 ounces). 8 Propulsion • Motor choice: AMW L777 • Thrust-to-weight ratio: 5.96 (average) • Rail exit velocity: 55.25 ft/s 9 Propulsion Full Scale Motor: Animal Works L777 (75mm) • Determined By Open Rocket Models 10 Propulsion Sub-Scale Motor: Aerotech J315 (54mm) • Determined By Open Rocket Models 11 Propulsion Full Scale Contingency Motor: Cesaroni L935 12 Propulsion Full Scale Contingency Motor: Cesaroni L935 13 Avionics & Recovery – Main Parachute: Fruity Chutes 84” Iris Ultra – Drogue Parachute: Rocketman 3’ Ballistic Mach II Chute – Recovery Harness: 50’ of ½” tubular Kevlar – Altimeters: 2x PerfectFlite StratoLogger – Down-body Camera: PD80 – Recovery Aids: • Garmin Astro DC-20 GPS System • BeepX Sonic Beacon 14 Avionics & Recovery Sled and Bay Design BeepX Sonic Beacon Altimeters Switches 9V Battery Holders BP Ejection Canister BeepX 12V 23A Battery CO2 Canister CD3 Ejection System Note: Aft Bulkhead is actually an aluminum bulkhead that interfaces with the motor casing and screws into the airframe 15 Avionics & Recovery –Apogee • CD3 CO2 ejection device • Black powder ejection charge • Drogue is released and main is held within the airframe by the main parachute containment harness. –750 ft AGL • Tender Descender releases the main and the drogue pulls it out of the airframe and deployment bag 16 Avionics & Recovery – Descent Rate • 64 ft/s under drogue • 15 ft/s under main – Kinetic Energy • Booster Section: 73.8 ft-lbs • Nosecone/Payload: 15.6 ft-lbs Avionics & Recovery – Altimeter test • Tested functionality of altimeters and ability to fire e-matches – CD3 independent test • Tested stand-alone functionality of CD3 system – Sub-scale ground test • Tested the ability of the CD3 system to eject the nosecone 18 Payload NASA SMD Mission Payload: • Measure atmospheric parameters • Will collect following data: – – – – – Pressure Temperature Relative Humidity Solar Irradiance Ultra-violet Radiation Payload 900MHz Transmitter Power Supply HASB HASB Arduino Control Arduino Control Light Sensor Power Supply Light Sensor Name Data Logger Data Logger Model Ultra-Violet Light Sensor SU-110 Logomatic v2 Serial SD Datalogger WIG-10216 Arduino Pro 3.3V/ 8Mhz DEV-09221 Polymer Lithium Ion Battery - 2000mAh PRT-08483 XBee Pro 900 XSC Wire Antenna WRL-09085 4GB microSD Card SDSDQ-4096-E11M High Altitude Sensing Board SEN-09944 ~Ambient Light Sensor TEMT-6000 ~Humidity Sensor HIH-4030 ~Pressure Sensor BMP-085 ~Accelerometer ADXl345 ~Temperature Sensor TMP-102 Quantity 2 2 2 2 1 2 2 2 2 2 2 2 Payload Payload Scientific Value: • Analyze collected information to profile atmospheric boundary layer • Determine stability and depth of atmospheric boundary layer • Construct a Skew-T diagram of the boundary layer as visual aid to determine weather severity [www.met.psu.edu] Safety & Quality Assurance • CO2 Canisters for CD3 System Pressure vs %Fill for varying Temperature – Manufactured to UL1191 Standard – Burst pressure: 7000psi – 75% Fill – 30 min @ 100 ⁰C, 15min @ 150 ⁰C 23 Safety & Quality Assurance Subsystem Component Verification Test Shear Pins Ground Testing (Feb.) Forward Motor Retainer Static Fire (Feb.) Avionics & Recovery Recovery System Ground Testing (Feb.) Propulsion Motor Static Fire (Feb.) Structures 24 Upcoming Milestones • Verification Testing as in explained in Appendix D: Test Matrix (February) • MDRA Launch (March 10-11) • METRA Launch (March 24) • FRR (March 26) 25 Educational Engagement • Discovery Space Museum Workshops – January 27, February 8 & 22, March 21 • Spikes Fest – February 12 • Park Forest Middle School STEM Fair – March 14 26 Expenses Full Scale Rocket Expenses by Subsystem Overall Club Expenses Section Total Full Scale $ 4,546.23 Subscale $ 2,612.09 Testing $ 1,040.66 Ground Support Equipment $ 2,461.91 Travel $ 3,815.00 Outreach $ 248.98 Total $ 14,724.87 Subsystem Structures & Aerodynamics Avionics & Recovery Payload Propulsion Total $ 1,853.99 $ 975.31 $ 1,266.93 $ 450.00 Total $ 4,546.23 27 Conclusion • Tests show that rocket is structurally sound and ejection/internal circuitry works. • Further testing for drogue parachute size, landing radius distance, and motor performance. 28 References [1] Fleeman, l.E., Tactical Missile Design – Second Edition, American Institute of Aeronautics and Astronautics, Inc., VA 2006 [2] www.fruitychutes.com [3] www.apogeerockets.com [4] www.met.psu.edu [5] www.wildmanrocketry.com [6] www.pro38.com [7] www.giantleaprocketry.com [8] www.eurorocketry.org 29