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Methane heat transfer investigationFuture high chamber pressure LOX/hydrocarbon booster engines require copper-base alloy main combustion chamber coolant channels similar to the SSME to provide adequate cooling and resuable engine life. Therefore, it is of vital importance to evaluate the heat transfer characteristics and coking thresholds for LNG (94% methane) cooling, with a copper-base alloy material adjacent to the fuel coolant. High-pressure methane cooling and coking characteristics were recently evaluated using stainless-steel heated tubes at methane bulk temperatures and coolant wall temperatures typical of advanced engine operation except at lower heat fluxes as limited by the tube material. As expected, there was no coking observed. However, coking evaluations need be conducted with a copper-base surface exposed to the methane coolant at higher heat fluxes approaching those of future high chamber pressure engines.
Document ID
19850004010
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cook, R. T.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:171199
NASA-CR-171199
ASR84-72
Accession Number
85N12318
Funding Number(s)
CONTRACT_GRANT: NAS8-34977
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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