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High capacity demonstration of honeycomb panel heat pipesThe feasibility of performance enhancing the sandwich panel heat pipe was investigated for moderate temperature range heat rejection radiators on future-high-power spacecraft. The hardware development program consisted of performance prediction modeling, fabrication, ground test, and data correlation. Using available sandwich panel materials, a series of subscale test panels were augumented with high-capacity sideflow and temperature control variable conductance features, and test evaluated for correlation with performance prediction codes. Using the correlated prediction model, a 50-kW full size radiator was defined using methanol working fluid and closely spaced sideflows. A new concept called the hybrid radiator individually optimizes heat pipe components. A 2.44-m long hybrid test vehicle demonstrated proof-of-principle performance.
Document ID
19890011820
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tanzer, H. J.
(Hughes Aircraft Co. Torrance, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:181776
NASA-CR-181776
Accession Number
89N21191
Funding Number(s)
CONTRACT_GRANT: NAS1-17674
CONTRACT_GRANT: NASA ORDER W-30851
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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