NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About Help Login
Back to Results
Experimental performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket enginesPerformance of liquid hydrogen-fluorine propellant combination in regeneratively cooled rocket engine
Document ID
19660024052
Document Type
Technical Memorandum (TM)
Authors
Douglass, H. W. (NASA Lewis Research Center Cleveland, OH, United States)
Hennings, G. (NASA Lewis Research Center Cleveland, OH, United States)
Price, H. G., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1959
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-87
Accession Number
66N33342
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REGENERATIVE COOLING
LIQUID
HYDROGEN FUEL
LIQUID PROPELLANT ROCKET ENGINE

Related Records

There are no records associated with this record.
No Preview Available