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Satellite thermal radiator heat dissipation structure has circuit component mountings and deployable thermal dissipater allowing second module full function

机译:卫星散热器的散热结构具有电路组件安装件和可展开的散热器,可实现第二个模块的全部功能

摘要

The thermal radiator is deployable from a satellite. The structure has a first module (22) with circuit component mounting. A second module (24) has circuit component mountings placed below the first module which are only fully functional in the thermal radiator deployed position. A thermal radiator (26,28) is deployed from the satellite dissipating the heat from the first and second unit.
机译:散热器可通过卫星部署。该结构具有带有电路组件安装的第一模块(22)。第二模块(24)具有放置在第一模块下方的电路部件安装件,其仅在散热器展开位置中完全起作用。卫星上部署了一个散热器(26,28),用于消散第一单元和第二单元的热量。

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