Optimal Thermal Design of a Multishield Thermal Protection System of Reusable Space Vehicles

We have solved the problem of the optimal thermal design of a multishield thermal protection system of reusable space vehicles due to the choice of the optimal position and materials of radiation shields.

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Bibliographic Details
Published in:Journal of engineering physics and thermophysics 2016-03, Vol.89 (2), p.528-533
Main Authors: Maiorova, I. A., Prosuntsov, P. V., Zuev, A. V.
Format: Article
Language:English
Subjects:
Classical Mechanics
Complex Systems
Engineering
Engineering Thermodynamics
Heat and Mass Transfer
Industrial Chemistry/Chemical Engineering
Materials selection
Optimization
Radiation
Radiation shielding
Reusable
Space ships
Space vehicles
Thermal design
Thermal protection
Thermodynamics
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Description
Summary:We have solved the problem of the optimal thermal design of a multishield thermal protection system of reusable space vehicles due to the choice of the optimal position and materials of radiation shields.
ISSN:1062-0125
1573-871X
DOI:10.1007/s10891-016-1406-8