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Thermal analysis of M552 experiment for materials processing in spaceAnalytical and experimental studies made of heat flow in the exothermic brazing unit in the M552 experiment are described. The emphasis of the studies was placed on heat flow in the tube and the sleeve during a period from ignition to the time when the brazing alloy solidifies. Experiments were made of three specimens tested in a ground-based laboratory. Heat flow was determined by thermocouples. The analytical study covered two phases: (1) the effect of reduced gravity on heat flow in the exothermic brazing unit; and (2) the development of analytical models. The major mode of heat transfer was conduction and the effect of gravity was minimal. Good agreements were obtained between experimental and analytical results indicating the soundness of the analytical models.
Document ID
19750005824
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Muraki, T.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Masubuchi, K.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Astronautics (General)
Report/Patent Number
NASA-CR-129043
Report Number: NASA-CR-129043
Accession Number
75N13896
Funding Number(s)
CONTRACT_GRANT: NAS8-28732
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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