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Active thermal load control system for spacecraft
Active thermal load control system for spacecraft
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机译:航天器的主动热负荷控制系统
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摘要
The system has a storage tank (18) in which working fluid (52) is stored. Heating and cooling units (82,64) are coupled to the tank through a conduit assembly (30). The conduit assembly performs transition of heat between heating and cooling units by passage of fluid conveyed through the conduit.
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