| 摘要 |
Equipment ( 20, 20 a) includes at least one electronic module ( 21 ) for the payload or the platform of a satellite (50) adapted to be supported by a structure ( 24 ) of the satellite, the satellite structure including a heat transfer system ( 44,10 ) for transporting dissipated heat to a radiator ( 51 ). The equipment includes at least transfer devices ( 22, 30, 31, 34, 341-345 ) for transferring heat dissipated by the electronic module and connectors ( 28, 34, 35, 37 ) for connecting the transfer devices to the heat transfer system ( 10 ) of the structure in such a manner as to enable the supply of heat exchange fluid ( 16 ) to the transfer devices and the transfer of heat dissipated by the electronic module to the radiator. A satellite structure includes an arrangement of equipments and a communication system for satellites, with particular application to the new generation of satellites with electrical propulsion.
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