A passive thermal system for use in a satellite and other aerospace applications includes a container having a heat-pipe working fluid disposed in a first chamber and a Phase Change Material (PCM) disposed in a second chamber that substantially surrounds the first chamber. The first chamber contains a wick for transporting the heat-pipe working fluid. The exterior of the first chamber has fins, etc., that extend into the PCM for heat spreading and increased interface area.
Passive Thermal System Comprising Combined Heat Pipe and Phase Change Material and Satellites Incorporating Same
2016-10-06
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
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