Trajectory Optimization for an APOLLO-Type Vehicle under Entry Conditions Encountered During Lunar Return
1967
41 pages
Report
Keine Angabe
Englisch
Spacecraft Trajectories & Flight Mechanics , Apollo spacecraft , Return-to-earth phase , Spacecraft reentry , Trajectory optimization , Acceleration , Altitude , Boundary , Earth , Entry , Heating , Lunar , Maneuver , Numerical , Optimization , Performance , Phase , Reentry , Return , Spacecraft , Trajectory
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