Hawaii - WCC

 5,280 ft  Carry a student payload  National CanSat program  No bigger than a 12 fl oz soda can  Mass no greater than 1 kg  USLI requires a dual deployment recovery

 Electronics in nose cone  Air brake system  Three fin design

5 phases  Boost phase  Coast phase Deployment of drogue chute at apogee  Initial decent rate  Approximately 60 ft/sec  Deployment of main chute at 500 ft  Slows approximately to less than 20 ft/sec  Close and intact recovery

Boost Phase

 Insert Apogee

 Insert Drogue Descent

 Insert 500’ Main

 Insert Main Descent

 G10 fiberglass  Motor  K560W by Aerotech  2,560 Newton seconds (thrust)x(burn time)  120 lbs of thrust  4.5 seconds of burn time