Dual conduction heat dissipating system for a spacecraft
US7048233B2 · kind B2 · utility
5Cited by
12References
29Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jul 8, 2004 |
| Grant date | May 23, 2006 |
| Priority date | — |
| Expiry date | Jul 8, 2024 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64G1/503
- WIPO fieldTransport
- WIPO sectorMechanical engineering
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.