发明名称 |
SPACECRAFT HEAT DISSIPATION SYSTEM |
摘要 |
A spacecraft is provided. The spacecraft comprises a plurality of heat generating electrical components. A first thermal radiator panel and a second thermal radiator panel are provided on the spacecraft, each panel being thermally coupled to the heat generating electrical components. Heat pipes are also provided. At least one first heat pipe is externally attached to the first thermal radiator panel and at least one second heat pipe is externally attached to the second thermal radiator panel. The at least one first heat pipe is thermally coupled to the at least one second heat pipe.
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申请公布号 |
US2010243817(A1) |
申请公布日期 |
2010.09.30 |
申请号 |
US20100730457 |
申请日期 |
2010.03.24 |
申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
MCKINNON DOUGLAS V.;MORAN TIMOTHY P. |
分类号 |
B64G1/58 |
主分类号 |
B64G1/58 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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