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Review of advanced radiator technologies for spacecraft power systems and space thermal controlA two-part overview of progress in space radiator technologies is presented. The first part reviews and compares the innovative heat-rejection system concepts proposed during the past decade, some of which have been developed to the breadboard demonstration stage. Included are space-constructable radiators with heat pipes, variable-surface-area radiators, rotating solid radiators, moving-belt radiators, rotating film radiators, liquid droplet radiators, Curie point radiators, and rotating bubble-membrane radiators. The second part summarizes a multielement project including focused hardware development under the Civil Space Technology Initiative (CSTI) High Capacity Power program carried out by the NASA Lewis Research Center and its contractors to develop lightweight space radiators in support of Space Exploration Initiative (SEI) power systems technology.
Document ID
19940032314
Document Type
Technical Memorandum (TM)
Authors
Juhasz, Albert J. (NASA Lewis Research Center Cleveland, OH, United States)
Peterson, George P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
SPACECRAFT PROPULSION AND POWER
Report/Patent Number
NAS 1.15:4555
NASA-TM-4555
E-8263
Funding Number(s)
PROJECT: RTOP 583-02-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19940032314.pdf STI