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Space shuttle orbiter heat pipe applications. Volume 1: SynopsisAn investigation was made to formulate and evaluate heat pipe applications for the space shuttle orbiter. Of the twenty-seven specific applications which were identified, a joint evaluation resulted in the selection of five of the most promising ones for prototype development. The formulation process is described, along with the applications which evolved. The bulk of the discussion deals with the top five applications: (1) heat pipe augmented cold rail; (2) avionics heat pipe circuit; (3) heat pipe/phase change material modular sink; (4) air-to-heat-pipe heat exchanger; and (5) heat pipe radiator for compartment temperature control. The philosophy, physical design details, and performance data are presented for each concept along with a comparison to the baseline design where applicable. A sixth application, heat pipe space radiator for waste heat rejection, was also recommended for prototype development.
Document ID
19720023257
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Alario, J. P.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Prager, R. C.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
SPR-14-VOL-1
NASA-CR-128497
Accession Number
72N30907
Funding Number(s)
CONTRACT_GRANT: NAS9-12034
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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