Spacecraft and Rockets
Аuthors
Abstract
Examine possible schemes of functioning spacecraft for prime orbital flight in case of ascent to unlocked intermediate orbits. Propose variants of final orbital injection and single-turn maneuvers. State principles of autonomous real-time choise flight variant in case of contingency.Keywords:
launcher, spacecraft, ascent, final orbital injection maneuver, contingency, single-turn trrajectory, control system, flight task, alternative choice of flight
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