Thermal Analysis of Trajectories of Return from the Moon Using Several Entries into the Atmosphere for Ballistic Capsule and Gliding Descent Vehicles

Author:

Leonov V. V.,Grishko D. A.,Airapetyan M. A.,Shvyrkina O. S.,Nikitin G. A.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical modeling of the temperature field on the surface of a ballistic capsule returning from a near-lunar orbit;AIP Conference Proceedings;2023

2. Anisotropic heat-shielding materials: Analysis of effectiveness of application for a ballistic capsule;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

3. Analysis of Thermal Protection Using an Anisotropic Material During the Return Capsule Descent;Solar System Research;2022-12

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