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Journal of Engineering Thermophysics

Published in:

01-09-2023

Calculation of Heat Loads in Analysis of Superorbital Entry of Spacecraft into Atmosphere of the Earth

Authors: D. L. Reviznikov, A. V. Nenarokomov, M. S. Konstantinov, I. A. Nikolichev, A. V. Morzhukhina, L. M. Chernova

Published in: Journal of Engineering Thermophysics | Issue 3/2023

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Abstract

Correlations for calculation of heat loads during a return of spacecraft at the second cosmic velocity are given. Analysis of the heat transfer for a model descent trajectory has been carried out. The convective and radiative heat fluxes, the relative heat transfer coefficient, and the radiative-equilibrium surface temperature have been calculated. The results obtained are a basis for design and optimization of the heat shield of spacecraft.

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Title: Calculation of Heat Loads in Analysis of Superorbital Entry of Spacecraft into Atmosphere of the Earth
Authors: D. L. Reviznikov
A. V. Nenarokomov
M. S. Konstantinov
I. A. Nikolichev
A. V. Morzhukhina
L. M. Chernova
Publication date: 01-09-2023
Publisher: Pleiades Publishing
Published in: Journal of Engineering Thermophysics / Issue 3/2023
Print ISSN: 1810-2328
Electronic ISSN: 1990-5432
DOI: https://doi.org/10.1134/S1810232823030050

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