NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Effect of thrust per element on combustion stability characteristics of hydrogen oxygen rocket enginesCoaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engine
Document ID
19680027043
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hannum, N. P. (NASA Lewis Research Center Cleveland, OH, United States)
Salmi, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Wanhainen, J. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-4851
Report Number: NASA-TN-D-4851
Accession Number
68N36515
Funding Number(s)
CONTRACT_GRANT: 128-31-06-05-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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