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The heat source for thermal module, and the space ship modular thermal platform null space ship which control, the thermal load from

机译:热量模块的热源,以及控制其热负荷的太空船模块化热量平台零空间船

摘要

Thermal module of the space ship (1) has, in order to control the thermal load which is generated by the heat source (3), 2 phaseless looping system (5) and thermal discharge or the expulsion system (13). 2 phaseless looping system (5) has, the solar collector (7), the thermal current regulator (10), the branching pipe conduit (6), the condenser (11). The condenser (11) with the thermal expulsion system (13) to be joined mutually thermally, 2 phaseless looping system (5) the thermal current regulator (10), portion of thermal load the condenser (11) to with to change direction from the heat source (3), the thermal expulsion system (13) the heat sink (14) to direct aforementioned thermal load from there, the heat source (3) to be cooled excessively, or in order or to prevent the fact that it becomes excessively low temperature, the heat source (3) temperature, through the branching pipe conduit (6), to convey the other portion of thermal load, the solar collector (7)You adjust by resetting, the thermal expulsion system (13), you are designed on the basis of the state of the highest temperature which can happen with the mission of the space ship.
机译:为了控制由热源(3)产生的热负荷,太空船(1)的热模块具有两个无相回路系统(5)以及热排放或驱逐系统(13)。图2所示的无相回路系统(5)具有太阳能收集器(7),热调节器(10),分支管道(6),冷凝器(11)。冷凝器(11)与排热系统(13)相互热连接,2个无相回路系统(5)的热电流调节器(10),冷凝器(11)的部分热负荷从改变方向热源(3),散热系统(13),散热器(14)从那里引导上述热负荷,要过度冷却的热源(3)或为了或防止其过度冷却的事实低温时,热源(3)的温度通过分支管道(6)传递热负荷的另一部分,即太阳能收集器(7)。通过重新设置,排热系统(13)根据太空船任务可能发生的最高温度状态进行设计。

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