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Flight Readiness Review. Team Hawaii. Vehicle Properties. Diameter ( in) 6 inches Length ( in) 127 inches Gross Liftoff Weight ( lb ) 50.25 lb Launch Lug/button Size large 1515 Motor Retention Aeropack 98 mm. Motor Properties. Motor Manufacturer AeroTech
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Flight Readiness Review Team Hawaii
Vehicle Properties • Diameter (in) 6 inches • Length (in) 127 inches • Gross Liftoff Weight (lb) 50.25 lb • Launch Lug/button Size large 1515 • Motor Retention Aeropack98 mm
Motor Properties • Motor Manufacturer AeroTech • Motor Designation L1500T • Max/Average Thrust (N/lb) 380 lbs/330 lbs • Total Impulse (N-sec/lb-sec) 5120 Ns/1150lbs-sec • Mass pre/post Burn (lb) 10.4 lb/5.2 lb
Stability • Center of Pressure (in from nose) 96.26 in • Center of Gravity (in from nose) 78.44 in • Static Stability Margin 2.97 • Thrust-to-Weight Ratio 7.18 • Rail Size (in) / Length (in) 0.5 in/120 in • Rail Exit Velocity (ft/s) 60 ft/s • Max Velocity (ft/s) 628.5 ft/s • Max Mach Number 0.7 • Max Acceleration(ft/s^2) 344 ft/s/s • Peak Altitude (ft) 5280 ft
Team Hawaii USLI 2011-2012 Booster (Scale 1:6; all inches) Main Chute Storage
Team Hawaii USLI 2011-2012 Drag Assembly Detail (Scale 1:1; all inches)
Lateral Drift Distance 0-2 mph wind 0.0 kg. payload: 202 ft. 0.5 kg payload: 197.6 ft. 1.0 kg payload: 186 ft. 1.5 kg payload: 150.4 ft. 2.0 kg payload: 136.2 ft. 3-7 mph wind 0.0 kg. payload: 920 ft. 0.5 kg payload: 788 ft. 1.0 kg payload: 758 ft. 1.5 kg payload: 692 ft. 2.0 kg payload: 645 ft. 8-14 mph wind 0.0 kg. payload: 2050 ft. 0.5 kg payload: 1800 ft. 1.0 kg payload: 1660 ft. 1.5 kg payload: 1610 ft. 2.0 kg payload: 1490 ft. 15-25 mph wind 0.0 kg. payload: 3890 ft. 0.5 kg payload: 3800 ft. 1.0 kg payload: 3390 ft. 1.5 kg payload: 3130 ft. 2.0 kg payload: 2960 ft.
Recovery • Altimeters • PerfectFlightMini Alt/WD • Featherflight Raven • Rocket Locators • GPSFlightSD900e • Transmitting Frequencies • GPSFlight is 912MHz • Beeline transmitter is 433.92 MHz,428.57 MHz
Parachutes Main - 7 grams black powder Drogue - 4 grams black powder Size 42 in diameter Altitude at Deployment (ft) apogee Velocity at Deployment (ft/s) 1.52 ft/s Terminal Velocity (ft/s) 75 ft/s Recovery Harness Length (ft) 40 ft • Size • 144 in diameter • Altitude at Deployment (ft) • 1100 ft • Velocity at Deployment (ft/s) • 75.7 ft/s • Landing Velocity (ft/s) • 21.8 ft/s • Recovery Harness Length (ft) • 20 ft • Both Chutes • Recovery Harness Material • Rip-stop Nylon • Harness Size/Thickness (in) • 1 in • Harness/Airframe Interfaces • 3/8 in U-bolt and qiuck links
Kinetic Energy Kinetic Energy During Descent (ft-lb) 3014 ft-lbs Kinetic Energy Upon Landing (ft-lb) • Section 1 74.5 ft-lbs • Section 2 68.0 ft-lbs • Section 3 60.5 ft-lbs • Section 4 24.2 ft-lbs
Deployment Test • 3/3/2012 Successful
Full Scale Low Power • 3/11/12 Successful • http://www.youtube.com/watch?v=3sZ3fvjzeWQ
Payload - ASTRID • Printed Circuit Board • Various Wires, Sockets, Risistors • Arduino Nano • Xbee-Pro 900 XSC • Micro Read Relay • BMP085 – Temperature, Pressure, Altitude • DS1307 Real Time Clock • DHT11 – Humidity • TSL2561 – Light Sensor x2 • TTL Serial JPEG – Camera • Micro SD storage
Payload - Walter • Printed Circuit Board • Various Wires, Sockets, Risistors • Three perpendicular coils around a non-magnetic sphere • 12-bit ADC • 3 Operation Amp • Micro SD storage • ArduinoNano • 3-axis accelerometer (comparison)
Mahalo Questions?