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

Spacecraft and Rockets


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

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



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.


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