التفاصيل البيبلوغرافية
| العنوان: |
Calculation of Heat Loads in Analysis of Superorbital Entry of Spacecraft into Atmosphere of the Earth. |
| المؤلفون: |
Reviznikov, D. L., Nenarokomov, A. V., Konstantinov, M. S., Nikolichev, I. A., Morzhukhina, A. V., Chernova, L. M. |
| المصدر: |
Journal of Engineering Thermophysics; Sep2023, Vol. 32 Issue 3, p467-481, 15p |
| مستخلص: |
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. [ABSTRACT FROM AUTHOR] |
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| قاعدة البيانات: |
Complementary Index |
