The invention provides a spacecraft thermal control structure and a spacecraft, provides a thermal control scheme which is compact in structure and can be directly installed, and can better meet the working temperature requirements of thermal insulation, refrigeration, heating and temperature equalization of a temperature-sensitive single machine.
本申请提供了一种航天器热控结构以及航天器,提供了一种结构紧凑、可直接安装的热控方案,且可以较好地满足温度敏感单机其隔热、制冷、加热和均温的工作温度需求。
Spacecraft thermal control structure and spacecraft
一种航天器热控结构以及航天器
2022-10-25
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
NTRS | 1973
NTIS | 1973
NTIS | 1989
|TIBKAT | 2012
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