University Student Launch Initiative
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1 University Student Launch Initiative HARDING UNIVERSITY Critical Design Review February 4, 2008
2 The Team Dr. Edmond Wilson Brett Keller Team Official Project Leader, Safety Officer Professor of Chemistry NAR Level 2 NAR Level 1 Box Harding University Searcy, AR 72149
3 Progress Since Preliminary Design Review: Design revisions (primarily in avionics bay) Major construction progress on airframe and electronics bay Publicity with local papers and statewide TV
4 Airframe: 94 (2.39 meter) length 3.1 diameter 54mm hybrid (Contrail Rockets I through K motors) Designed to reach target altitude of one mile
5 Aft section: 34 long 54mm motor mount tube Fins are composed of a composite sandwich: - 1/8 inch 3-ply birch plywood - 6 oz. fiberglass - carbon fiber - 6 oz fiberglass - 1/8 inch 3-ply birch plywood Fin joint with motor mount tube was reinforced with carbon fiber, as pictured.
6 Middle tube section (20 in length): Aft 10 section houses scientific payload (spectrometer) which gathers data on the exhaust plume via a fiber optic cable Forward 10 section houses recovery electronics on a core electronics support structure surrounded by removable, transparent acrylic tubing.
7 Recovery electronics section: clear acrylic tubing around internal support structure (threaded rods not pictured)
8 Recovery electronics section: clear acrylic tubing around internal support structure (threaded rods not pictured). One 9 volt battery installed.
9 Forward body section 28 tube and nose cone Contains drogue parachute, main parachute, Chute Tamer deployment device
10 Side View with SolidWorks 2007 Left to right: nose cone, 28 parachute section, 4 transition section, 10 clear acrylic electronics bay (with internal structure shown), 10 scientific payload bay, 34 main aft tube with fins.
11 3-D Rendering of Forward Section with SolidWorks D Rendering of Aft Section with SolidWorks 2007
12 3-D Isometric Rendering with SolidWorks 2007
13 Motor: Contrail Rockets 54mm J-234 (total impulse of 1033 Newtonseconds). Nitrous oxide oxidizer, stored in portable tank (complete filling system owned by Harding) Rocket design can accommodate up to 36 long 54mm motor
14 Electronics include: Perfectflite MAWD logging altimeter unit Boostervision wireless color 2.4Ghz Wireless Micro Camera will record in-flight video. R-DAS flight computer (measurements and transmission of telemetry) backup for parachute deployment and data logging stores information from spectrometer GPS board telemetry transmitting and receiving capabilities.
15 Cutaway diagram of custombuilt spectrometer in avionics bay.
16 Experiments to be flown in rocket: Custom spectrometer (based on a commercially available SpectraWiz compact spectrometer) to study hybrid rocket exhaust plume via fiber optic cable R-DAS GPS system (allowing in-flight tracking of the rocket) R-DAS accelerometer and altimeter components. Perfectflite altimeter.
17 Experiments to be flown in rocket (continued): Onboard spectrometer will yield spectral data from the hybrid rocket exhaust plume in flight. Combustion intermediates such as hydroxyl radical will be identified in the spectra. In-flight video will allow for frame-by-frame analysis synchronized with the spectrometer and positional data
18 Project goals: 1. Build a rocket capable of reaching 5280 feet and capable of being reasonably retrieved via dual deployment recovery techniques. 2. Build a working science package including a spectrometer that can be used to analyze the plume gradients. 3. Complete construction, testing, and flights safely, on schedule, and on budget. 4. Share information about science, rocketry, and NASA with local media and schoolchildren through outreach programs
19 2. Outreach Harding USLI team has been featured several times in Searcy s Daily Citizen newspaper. Project Leader Brett Keller presented this poster at the Arkansas INBRE scientific conference and won 2 nd place in the physics division.
20 2. Outreach Flying Bison Outreach Coordinator Megan Bush and Harding University President David Burks appeared on Channel 7 s Good Morning Arkansas, Arkansas most-viewed morning show, to talk about the USLI competition.
21 3. Project plan January: Bench testing of spectrometer with R-DAS and other electronics components February 4: Critical Design Review (tentative) February 9: Memphis launch; test fly Perfectflite MAWD in Dr. Wilson s Level 1 rocket with hybrid I motor. February: Complete airframe construction of competition vehicle March 8: Memphis launch: test flight of competition vehicle on hybrid I motor March 31: Flight Readiness Review Presentation Slides and FRR Report due April 7: Flight Readiness Review (tentative) April 12: Memphis launch: test flight of competition vehicle on J-234 hybrid motor (full power, full scale test flight) April 18: Flight Hardware Check (tentative) April 19: Launch Day (Rain date of April 20) May 12: Post-Launch Assessment Review
22
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