Dual conduction heat dissipating system for a spacecraft

Details Dual conduction heat dissipating system for a spacecraft Dual conduction heat dissipating system for a spacecraft

2006-05-23

2006-05-23

Barefoot, Galen (Department: 3644)

Aeronautics and astronautics

Spacecraft

With shield or other protective means

C165S041000

Reexamination Certificate

active

07048233

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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