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Heat pipe radiators for spaceAnalysis of the data heat pipe radiator systems tested in both vacuum and ambient environments was continued. The systems included (1) a feasibility VCHP header heat-pipe panel, (2) the same panel reworked to eliminate the VCHP feature and referred to as the feasibility fluid header panel, and (3) an optimized flight-weight fluid header panel termed the 'prototype.' A description of freeze-thaw thermal vacuum tests conducted on the feasibility VCHP was included. In addition, the results of ambient tests made on the feasibility fluid header are presented, including a comparison with analytical results. A thermal model of a fluid header heat pipe radiator was constructed and a computer program written. The program was used to make a comparison of the VCHP and fluid-header concepts for both single and multiple panel applications. The computer program was also employed for a parametric study, including optimum feeder heat pipe spacing, of the prototype fluid header.
Document ID
19760015408
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sellers, J. P.
(Tuskegee Inst. AL, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AR-3
HP-2
NASA-CR-147659
Report Number: AR-3
Report Number: HP-2
Report Number: NASA-CR-147659
Accession Number
76N22496
Funding Number(s)
CONTRACT_GRANT: NAS9-13844
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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