aae 450 spring 2008 tim lorenzana 1/16/2008 avionics recovery/termination
TRANSCRIPT
AAE 450 Spring 2008
Tim Lorenzana1/16/2008
AvionicsRecovery/Termination
AAE 450 Spring 2008
Rocket Recovery Parachute Impact System
– Airbags Retro Rockets Rotating Wing
– Helicopter Action
Avionics
Nylon
496.05grams/meter $12.14meter
Launch Vehicle Mass 100.5kg
Parachute Diameter 1.06meters
Parachute Mass 2.22kg
Parachute Cost $54.27
AAE 450 Spring 2008
Rocket Termination Federal Aviation Regulations Require Our Launch
Vehicle Have the Capability to Self Destruct Before Causing Damage or Harm to People or Property.
Avionics
Future Work Further Analysis of Recovery Options Greater Understanding of
Termination Requirements and Guidelines
AAE 450 Spring 2008
Basic Parachute CalculationsDrag Force
Weight
At Full Chute Deployment;
Descent Velocity
Chute Diameter
Avionics
2
2
1SVCD d
mgF
2
2
1SVCmg d
SC
mgV
d2
S
Diameter 2