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Space thermal control developmentThe results of experimental investigations on a number of various phase change materials (PCMs) and PCMs in combination with metals and other materials are reported. The evaluations include the following PCM system performance characteristics: PCM and PCM/filler thermal diffusivities, the effects of long-term thermal cycling, PCM-container compatibility, and catalyst effectiveness and stability. Three PCMs demonstrated performance acceptable enough to be considered for use in prototype aluminum thermal control devices. These three PCMs are lithium nitrate trihydrate with zinc hydroxy nitrate catalyst, acetamide, and myristic acid. Of the fillers tested, aluminum honeycomb filler was found to offer the most increase in system thermal diffusivity.
Document ID
19720007297
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hoover, M. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Grodzka, P. G.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Oneill, M. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
LMSC/HREC-D225500
NASA-CR-150724
Report Number: LMSC/HREC-D225500
Report Number: NASA-CR-150724
Accession Number
72N14947
Funding Number(s)
CONTRACT_GRANT: NAS8-25183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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