Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere |
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| Authors: | A V Bobylev A A Dyad’kin V I Kobzev V M Poedinok A G Reshetin S N Suprunenko V A Jaroshevskii |
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| Institution: | (1) Zhukovsky Central Institute of Aerohydrodynamics, Zhukovsky, Moscow oblast, 140160, Russia;(2) “Energiya” Rocket and Space Corporation, Korolev, Moscow oblast, Russia |
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| 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. |
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| Keywords: | 45 40 Gj |
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