On Developing the Design of the Protective Heat Shield for the Interhelio-Zond Spacecraft
- Authors: Alekseev S.V.1, Aksenova I.V.1, Ivanova E.K.1, Kharitonova E.V.1, Lokhov A.A.2
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Affiliations:
- Lavochkin Association
- Ural Research and Development Institute of Composite Materials (UNIIKM)
- Issue: Vol 52, No 7 (2018)
- Pages: 680-683
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/171228
- DOI: https://doi.org/10.1134/S003809461807002X
- ID: 171228
Cite item
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.
About the authors
S. V. Alekseev
Lavochkin Association
Author for correspondence.
Email: nio27@laspace.ru
Russian Federation, Khimki, 141402
I. V. Aksenova
Lavochkin Association
Email: nio27@laspace.ru
Russian Federation, Khimki, 141402
E. K. Ivanova
Lavochkin Association
Email: nio27@laspace.ru
Russian Federation, Khimki, 141402
E. V. Kharitonova
Lavochkin Association
Email: nio27@laspace.ru
Russian Federation, Khimki, 141402
A. A. Lokhov
Ural Research and Development Institute of Composite Materials (UNIIKM)
Email: nio27@laspace.ru
Russian Federation, Perm, 614014
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