On Developing 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.

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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