The results are presented of a study to show the effect on flyback trajectories of constant inertial attitude during the fuel dissipation phase of a return-to-launch-site abort. It is shown that the value of the constant inertial attitude can be chosen to shape the flyback trajectory.
Return-to-launch-site trajectory shaping
17.10.1975
Report
Keine Angabe
Englisch
Return-to-Launch-Site Trajectory Shaping
NTIS | 1975
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