NASA NTRS · 19870008358
Rotating bubble membrane radiator for space applications
Abstract
An advanced radiator concept for heat rejection in space is described which uses a two-phase working fluid to radiate waste heat. The development of advanced materials and the large surface area per mass makes the Bubble Membrane Radiator an attractive alternative to both conventional heat pipes and liquid droplet radiators for mid to high temperature applications. A system description, a discussion of design requirements, and a mass comparison with heat pipes and liquid droplet radiators are provided.
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Webb, Brent J.. 1986-05-01. Rotating bubble membrane radiator for space applications. https://ntrs.nasa.gov/citations/19870008358
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