The effect of gravitational stress on the diffusion of liquids.
New team
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February 17Full scale vehicle completed February 18Full scale
test flight #1 (1/2 impulse) March 17Full scale test flight #2
(full impulse) April 19/20Flight hardware and safety checks April
21Launch day, full scale fight #3 April 28/29Full scale flight #4
(rain date flight)
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Event 1: Ignition at 0s, 0ft Event 2: Burnout at 2.24s, 1000ft
Coast Event 3: Apogee at 16s, 4502ft Drogue descent Event 4: Main
parachute deployment at 84s, 700ft Event 5: Landing at 110s, 0ft
Apogee prediction updated based on data from full scale
full-impulse flight (C d = 0.65 ): 4502 ft Apogee prediction
updated based on data from full scale full-impulse flight (C d =
0.65 ): 4502 ft
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Motor ignition Stable flight Altitude of 5,280 feet AGL reached
but not exceeded (most current prediction: 4502ft) Both drogue and
main parachute deployed Vehicle returns to the ground safely with
minimal damage Safe recovery of the booster
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CP 83.1 from nosecone CG 65.6 from nosecone Static margin 5.5
calibers Length 108 Diameter 5.5(body tube), 4(booster) Liftoff
Weight 21 lbs with AT-K1050W Motor Aerotech K1050W
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LetterPart ANosecone BMain Parachute CDrogue Parachute DPayload
Bay ETransition FMotor Mount GFins
