Abstract
Thermal management technology is the important means to optimize the design of thermal control system and maintain the manned thermal environment within the docking spacecraft combination. Through the thermal characteristic analysis of com- bination between target spacecraft and manned spacecraft, the thermal management design and simulated model basing on inter cabin ventilation were proposed. Results of simulation and thermal balance tests and orbital data show that velocity distribution satisfied the need and the air temperature and humidity were in target area. Base on simulation and tests, the thermal management design of manned combination was proved. The paper concluded the thermal management technology for space station.
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