NASA Rocket Team's Innovative Magnetic G-Force Remediation Solution
This presentation covers the preliminary design, goals, and payloads of NASA's Cedar Park Rocket Team, focusing on the use of magnetic fields to mitigate G-forces during rocket launches. The team's innovative solutions include magnetic dampening and advanced recovery systems to ensure successful missions. Explore their rocket requirements, design specifications, and payload ideas for a fascinating glimpse into cutting-edge aerospace technology.
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Presentation Transcript
NASA SLI Cedar Park Rocket Team MAGNETIC G-FORCE REMEDIATION
Our Rocket Requirements The rocket must reach 5,280 feet above ground level The Rocket payload should delay or equalize the effects of G-Forces on the inside container by using magnetic fields
Our preliminary Rocket design and Goals Rocket stability margin: 1.55 Center of gravity: 35.99 in Center of diametric pressure: 45.68 in
Rocket Launch Thrust/Acceleration/Altitude 7000 6000 5000 4000 3000 2000 1000 0 0.61 1.22 1.83 2.44 3.05 3.66 4.27 4.88 5.49 6.71 7.32 7.93 8.54 9.15 9.76 10.37 10.98 11.59 12.2 12.81 13.42 14.03 14.64 15.25 15.86 16.47 17.08 17.69 18.3 18.91 6.1 0 -1000 Altitude Feet Thrust N y-Acceleration Feet/sec/sec
Parts and Materials Motor: Aerotech K560W Carbon Fiber fins Fiberglass body with epoxy bonds Plastic nosecone
Recovery System Redundant black powder charges, circuit systems, and batteries for both the drogue and main parachutes.
Initial Payload Ideas Carbon Nano wire test electrical current while experiencing G-forces Carbon Nano wire stress test under G-forces Slime mold growth rate after experiencing G- forces
Final Payload choice Magnetic Dampening Using magnetic levitation to diminish G-forces experienced by the payload
