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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2008




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.93 Weltraumforschung / 39.00 Astronomie: Allgemeines / 55.60 Raumfahrttechnik
    Local classification TIB:    770/3520/8000



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

    Bobylev, A. V. / Dyad’kin, A. A. / Kobzev, V. I. et al. | Springer Verlag | 2008


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    Mooij, E. / Hanninen, G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009



    Use of aerodynamic lift during entry into earth's atmosphere

    Lees, L. / Hartwig, F.W. / Cohen, C.B. | Engineering Index Backfile | 1959