Numerical method of modelling of external heat exchange of the space vehicle with any form of external surfaces

Spacecraft and Rockets


Аuthors

Kolesnikov A. V., Paleshkin A. V.*

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: paleshkin@mai.ru

Abstract

The method of calculation of external heat exchange of the space vehicle developed by authors, based on approximation of external surfaces of a space vehicle and visible of a space vehicle a site of a surface of a planet many-sided surfaces with elementary triangular sides and on the subsequent numerical preliminary treatment ofpossible effect of mutual shielding these sides from proceeding from the Sun and a radiation planet is stated.

Keywords:

the Space vehicle, heat exchange by radiation, the Sun, a planet.

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