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Deployable Heat Pipe RadiatorA 1.2- by 1.8-m variable conductance heat pipe radiator was designed, built, and tested. The radiator has deployment capability and can passively control Freon-21 fluid loop temperatures under varying loads and environments. It consists of six grooved variable conductance heat pipes attached to a 0.032-in. aluminum panel. Heat is supplied to the radiator via a fluid header or a single-fluid flexible heat pipe header. The heat pipe header is an artery design that has a flexible section capable of bending up to 90 degrees. Radiator loads as high as 850 watts were successfully tested. Over a load variation of 200 watts, the outlet temperature of the Freon-21 fluid varied by 7 F. An alternate control system was also investigated which used a variable conductance heat pipe header attached to the heat pipe radiator panel.
Document ID
19750017016
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Edelstein, F.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-143863
DHPR-75-13
Report Number: NASA-CR-143863
Report Number: DHPR-75-13
Accession Number
75N25088
Funding Number(s)
CONTRACT_GRANT: NAS8-29905
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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