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High thermal-transport capacity heat pipes for space radiatorsThis paper presents the results of performance tests of several dual-slot heat pipe test articles. The dual-slot configuration has a very high thermal transport capability and has been identified as a very promising candidate for the radiator system for the NASA Space Station solar dynamic power modules. Two six-foot long aluminum heat pipes were built and tested with ammonia and acetone. A 20-ft long heat pipe was also built and tested with ammonia. The test results have been compared with performance predictions. A thermal transport capacity of 2000 W at an adverse tilt of 1 in. and a 1000 W capacity at an adverse tilt of 2 in. were achieved on the 20-ft long heat pipe. These values are in close agreement with the predicted performance limits.
Document ID
19880033928
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlson, Albert W.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Gustafson, Eric
(Grumman Aerospace Corp. Bethpage, NY, United States)
Roukis, Susan L.
(Grumman Corp. Space Systems Div., Bethpage, NY, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
SAE PAPER 871509
Accession Number
88A21155
Funding Number(s)
CONTRACT_GRANT: NAS3-24665
Distribution Limits
Public
Copyright
Other

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