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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

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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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Authors and Affiliations

  1. Zhukovsky Central Institute of Aerohydrodynamics, Zhukovsky, Moscow oblast, 140160, Russia

    A. V. Bobylev, V. I. Kobzev, V. M. Poedinok & S. N. Suprunenko

  2. “Energiya” Rocket and Space Corporation, Korolev, Moscow oblast, Russia

    A. A. Dyad’kin & A. G. Reshetin

Authors
  1. A. V. Bobylev
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  2. A. A. Dyad’kin
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  3. V. I. Kobzev
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  4. V. M. Poedinok
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  5. A. G. Reshetin
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  6. S. N. Suprunenko
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  7. V. A. Jaroshevskii
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Additional information

Original Russian Text © A.V. Bobylev, A.A. Dyad’kin, V.I. Kobzev, V.M. Poedinok, A.G. Reshetin, S.N. Suprunenko, V.A. Jaroshevskii, 2008, published in Kosmicheskie Issledovaniya, 2008, Vol. 46, No. 1, pp. 75–89.

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Bobylev, A.V., Dyad’kin, A.A., Kobzev, V.I. et al. Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere. Cosmic Res 46, 74–89 (2008). https://doi.org/10.1134/S0010952508010097

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  • DOI: https://doi.org/10.1134/S0010952508010097

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