Abstract We consider the problems of control of the angular and trajectory motion of the Kliper re-entry vehicle. This spacecraft with a moderate hypersonic lift-to-drag ratio is designed according to the load-carrying frame scheme. Gas-dynamic engines, a split balancing flap, and an air brake are used as mounting devices of control.
Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere
Cosmic Research ; 46 , 1
2008
Article (Journal)
English
BKL: | 50.93 Weltraumforschung / 39.00 Astronomie: Allgemeines / 55.60 Raumfahrttechnik | |
Local classification TIB: | 770/3520/8000 |
Distributed Global Trajectory Optimization of a Moderate Lift-to-Drag Re-Entry Vehicle
British Library Conference Proceedings | 2009
|Use of aerodynamic lift during entry into earth's atmosphere
Engineering Index Backfile | 1959
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