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 ; 74-89
2008-02-01
16 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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