Shock Tube Simulation of Radiative Heat Flux to the Space Vehicle Surface During its Reentering the Planetary Atmospheres

Authors

N. N. KOUDRIAVTSEV
A. M. SUKHOV

Abstract

Shock tube simulation of radiative heat flux due to space vehicle entry into a planetary atmosphere has been carried out and results are presented.

DOI

-

First Page

909

Last Page

914

Recommended Citation

KOUDRIAVTSEV, N. N, & SUKHOV, A. M (1996). Shock Tube Simulation of Radiative Heat Flux to the Space Vehicle Surface During its Reentering the Planetary Atmospheres. Turkish Journal of Physics 20 (8): 909-914. https://doi.org/-