Slide 1

The effect of gravitational stress on the diffusion of liquids. New team

Slide 2

Slide 3

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)

Slide 4

Slide 5

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

Slide 6

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

Slide 7

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

Slide 8

LetterPart ANosecone BMain Parachute CDrogue Parachute DPayload Bay ETransition FMotor Mount GFins

Slide 9