NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Experimental performance of gaseous hydrogen and liquid oxygen in uncooled 20,000-pound-thrust rocket enginesGaseous hydrogen and liquid oxygen experiments in uncooled 20,000-pound-thrust rocket engines
Document ID
19650023661
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Kinney, G. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Kutina, F. J., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Rothenberg, E. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1959
Subject Category
Propellants
Report/Patent Number
NASA-MEMO-4-8-59E
Accession Number
65N33262
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYDROGEN
ROCKET THRUST
LOX-HYDROGEN ENGINE
LIQUID OXYGEN /LOX/
LIQUID PROPELLANT ROCKET ENGINE
GAS
No Preview Available