James Goppert Week 6: February 22 th , 2007. Aerodynamics: Reentry Optimization Dynamics and Control: Communication Satellite Orbits. Taxi Capsule Vehicle Reentry. Assumptions Delta V from HMO: 500 [m/s] TCV Total Mass: 30 [mt] (after Delta V burn from HMO) Landing close to equator
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Aerodynamics: Reentry Optimization
Dynamics and Control: Communication Satellite Orbits
Taxi Capsule Vehicle Reentry
Delta V from HMO: 500 [m/s]
TCV Total Mass: 30 [mt] (after Delta V burn from HMO)
Landing close to equator
Actual: 4.78 [m/s]
Maximum : 6.7 [m/s] (15 mph)
Rocket Equation Prediction: 2.808 [mt] (Jamison)Taxi Capsule Vehicle Reentry
Max g load: 12g’s
Altitude: 300 [m]
Time: 60 [s]
1 High Mach Drogue
2 Low Mach Drogue
3 Main ChutesTaxi Capsule Vehicle Reentry
Max g Load
James GoppertWeek 4: February 22th, 2007
F_t_b = [0;0;0]
F_t_b = k_th*[h_hover-h;0;0]-...
F_t_b = k_ln*[0-h;0;0]-...