Heat exchange via radiation dispersed thermal liquid of spacecrafts

Space technics and technology


Konioukhov G. V.1, Koroteev A. A.2*

1. Keldysh Research Centre, 8, Onezhskaya str., Moscow, 125438, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: chkt@yandex.ru


Method of liquid droplet radiator's shroud radiative cooling calculation is presented. In the case of optical transparency in one direction, the possibilities of simplified method's realization are considered.


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