A detailed performance evaluation of the Abort Region Determinator (ARD) module design was provided in support of OFT-1 ascent and OFT-1 intact launch aborts. The evaluation method used compared ARD results against results obtained using the full-up Space Vehicle Dynamic Simulations program under the same conditions. Results were presented for each of the three major ARD math models: (1) the ascent numerical integrator; (2) the mass model, and (3) the second stage predictor as well as the total ARD module. These results demonstrate that the baselined ARD module meets all design objectives for mission control center orbital flight test launch/abort support.
Abort Region Determinator (ARD) module feasibility report. Mission planning, mission analysis and software formulation
1976-10-17
Report
No indication
English
Mars Mission Abort Considerations
NTRS | 2024
|Mars Mission Abort Considerations
NTIS | 2024
|