HEATPIPES AND VAPOUR CHAMBERS FOR SATELLITE THERMAL BALANCE.
Abstract
Heatpipes and vapour chambers, employing the principles of vapour heat transport, may be constructed with thermal conductances far higher than a solid metal structure with similar dimensions. This report describes the operation of these devices, and obtains quantitative estimates of the performance to be expected from them. It then discusses some of the ways in which they may be used to assist satellite thermal control. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1969
- Accession Number
- AD0696468
Entities
People
- C. J. Savage
Organizations
- Royal Aircraft Establishment