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Monoball energy transfer: Test reportAn aluminum platform serves as a storage shelf for experiments transported on the space shuttle. This platform is attached to the shuttle storage area through several supports, each consisting of an attachment fitting, a monoball bearing, a clevis pin and a support strut. The experiments must be temperature controlled during and after launch. Consequently, heat loss through the plate, attachment fitting, monoball bearing, and strut are important. The overall conductance of the monoball bearing was determined by an experimental method of heating the outer ring with a nichrome resistance wire and cooling the inner ball with propylene glycol. Temperature differences across the bearing were measured for various heat fluxes. The overall conductance is 0.42 Watts/C (0.80 BTU/hr F), This yields a 16 watt loss for a 38 C temperature difference across the bearing.
Document ID
19860017079
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wessling, F. C.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:176812
NASA-CR-176812
Report Number: NAS 1.26:176812
Report Number: NASA-CR-176812
Accession Number
86N26551
Funding Number(s)
CONTRACT_GRANT: NAG8-046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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