Dual conduction heat dissipating system for a spacecraft
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United States of America Patent
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May 23, 2006
Issued Date -
N/A
app pub date -
Jul 8, 2004
filing date -
Jul 11, 2003
priority date (Note) -
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Abstract
A system dedicated to dissipating heat produced by amplifier tubes of a spacecraft comprises a radiating panel installed substantially parallel to the amplifier tubes and thermally coupled to them to radiate to the outside a portion of the heat that they produce, a radiating receptacle whose walls define a housing adapted to receive the collectors of the amplifier tubes, and preferably a heat distributor that is preferably interleaved between the collectors and one wall of the receptacle to distribute the heat that the collectors produce between the collectors and the wall.
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