Spectral Emissivity of a Reentry Orbital Space Vehicle

S. T. Surzhikov

doi:10.1134/S1028335818100038

Spectral Emissivity of a Reentry Orbital Space Vehicle

Authors: Surzhikov S.T.¹^,2
Affiliations:
1. Ishlinsky Institute for Problems in Mechanics, Russian Academy of Sciences
2. Dukhov All-Russia Research Institute of Automation
Issue: Vol 63, No 10 (2018)
Pages: 397-401
Section: Physics
URL: https://journals.rcsi.science/1028-3358/article/view/192491
DOI: https://doi.org/10.1134/S1028335818100038
ID: 192491

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Abstract
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Abstract

The problem of the spectral emissivity of the Soyuz-TM descent module during its entry into the dense layers of the atmosphere at altitudes of 90–45 km with an orbital velocity has been solved. The results of three-dimensional numerical simulations are compared with experimental data.

Keywords

Descent Module (DM), Spectral Optical Properties, Compressed Layer, Aerodynamic Shield, Surface Emission Factor

About the authors

S. T. Surzhikov

Ishlinsky Institute for Problems in Mechanics,
Russian Academy of Sciences; Dukhov All-Russia Research Institute of Automation

Author for correspondence.
Email: surg@ipmnet.ru
Russian Federation, pr. Vernadskogo 101, Moscow, 119526; Moscow, 127055

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