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Techniques associated with thermal-vacuum testing of the OAO-C heat pipesThe mechanical problems associated with testing the two high-heat load pipes are discussed. One of these pipes was tested three times before being accepted. The first test resulted in the discovery of non-condensable hydrogen gas, which prevented the pipe from functioning properly. The second test was a repeat of the first, to see if all the gas had been removed. The third test was to see if any changes had occurred to the pipe as a result of saddle modifications. Saddle modifications were necessary because the epoxy binding agent between the saddles and the pipe had decomposed during the testing. The test problems discussed deal with the specially designed heat-removal devices, the mobile tilt table, the table position indicator, and the heat input mechanisms, all of which were necessary to conduct a high-heat load, thermal-vacuum test. The final results showed that the techniques used were adequate for thermal-vacuum testing of heat pipes.
Document ID
19720014658
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marshburn, J. P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Publication Information
Publication: Space Simulation
Subject Category
Thermodynamics And Combustion
Report/Patent Number
PAPER-80
Accession Number
72N22308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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