Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere

Details Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere

Feb 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008cosre..46...74b&link_type=abstract

Cosmic Research, Volume 46, Issue 1, pp.74-89

Physics

45.40.Gj, Ballistics

Scientific paper

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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