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Computer Hydrogen-Flow Splits In A Rocket EngineReport presents study of flows of hydrogen (as both coolant and fuel) along various paths in fuel injector of rocket engine. Study included computational simulations of flows.
Document ID
19950070436
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Romine, W. Dennis (Rockwell International Corp.)
Date Acquired
August 16, 2013
Publication Date
November 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 11
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-30024
ISSN: 0145-319X
Report Number: MFS-30024
Accession Number
95B10615
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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