In this paper, we introduce a microwave absorbing heat flow simulation system for vacuum thermal test of large microwave antenna on spacecraft, which is mainly used for the vacuum thermal test of spacecraft microwave antenna. This method of microwave absorbing external heat flux not only meets the requirement of vacuum thermal test, but also can control the temperature of the antenna different part separately, and effectively simulate the temperature change of the antenna on the orbit.
Microwave Absorbing Heat Flow Simulation System for Vacuum Thermal Test of Large Microwave Antenna
01.07.2018
8431371 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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