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Heat pipe flight experimentsOAO 3 heat pipe flight experiments to check out weightlessness behavior are reported. Tested were a hollow channel screen system with helical grooves, a heat pipe with a wicking system of horizontal grooves, and a spiral artery pipe with multichannel fluid return to the evaporator. Flight experiment data proved that all heat pipe geometries containing wicking systems provided uninterrupted fluid return to the condensators during weightlessness and sufficient cooling for isothermalizing optical instruments onboard OAO.
Document ID
19730019094
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ollendorf, S.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Significant Accomplishments in Technol., 1972
Subject Category
Thermodynamics And Combustion
Accession Number
73N27826
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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