DESIGNING PASSIVE THERMAL CONTROL SYSTEM WITH A CAPACITY OF UP TO 3 kW BY HEAT PIPES AND ACTIVE HEATING ELEMENTS FOR A SPACECRAFT

Autor: Oleg V. Shilkin, Anatoliy P. Kolesnikov, Aleksandr A. Kishkin, Aleksandr A. Zuev, Aleksandr V. Delkov
Rok vydání: 2022
Zdroj: Vestnik Moskovskogo aviatsionnogo instituta. 29:67-80
ISSN: 0869-6101
DOI: 10.34759/vst-2022-1-67-80
Databáze: OpenAIRE