Numerical modeling of the temperature field on the surface of a ballistic capsule returning from a near-lunar orbit.

Autor: Zarubin, V. S., Leonov, V. V.
Předmět:
Zdroj: AIP Conference Proceedings; 2023, Vol. 2849 Issue 1, p1-5, 5p
Abstrakt: This paper presents the solution to a non-linear non-stationary heat transfer problem in a double-layer heat shield coating on a metal hemispherical shell with an axisymmetric distribution of the heat flow density over the outer coating surface. The coating's outer layer material has thermal conductivity anisotropy characterized by a ratio of the thermal conductivity coefficients along and across the layer. The resulting solution has been used to quantitatively assess the thermal behavior of such a coating on a ballistic capsule when it enters the dense layers of the Earth's atmosphere with a velocity close to a parabolic one, with a single preliminary dipping into the atmosphere and entry into a near-earth orbit before the final stage of descent. [ABSTRACT FROM AUTHOR]
Databáze: Complementary Index