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On Develo** the Design of the Protective Heat Shield for the Interhelio-Zond Spacecraft

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Abstract

This article describes the design of the protective heat shield for the Interhelio-Zond spacecraft, accepted for full-scale engineering development. The material proposed for making the shield’s parts is a carbon-carbon composite material (CCCM). The technology of making and mating of the CCCM shield parts is determined.

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Authors and Affiliations

  1. Lavochkin Association, Khimki, 141402, Russia

    S. V. Alekseev, I. V. Aksenova, E. K. Ivanova & E. V. Kharitonova

  2. Ural Research and Development Institute of Composite Materials (UNIIKM), Perm, 614014, Russia

    A. A. Lokhov

Authors
  1. S. V. Alekseev
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  2. I. V. Aksenova
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  3. E. K. Ivanova
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  4. E. V. Kharitonova
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  5. A. A. Lokhov
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Corresponding author

Correspondence to S. V. Alekseev.

Additional information

Original Russian Text © S.V. Alekseev, I.V. Aksenova, E.K. Ivanova, E.V. Kharitonova, A.A. Lokhov, 2017, published in Vestnik NPO imeni S.A. Lavochkina, 2017, No. 1, pp. 64–67.

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Alekseev, S.V., Aksenova, I.V., Ivanova, E.K. et al. On Develo** the Design of the Protective Heat Shield for the Interhelio-Zond Spacecraft. Sol Syst Res 52, 680–683 (2018). https://doi.org/10.1134/S003809461807002X

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  • DOI: https://doi.org/10.1134/S003809461807002X

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