NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About Help Login
Back to Results
Use of highly reactive chemical additives to improve afterburner performance at altitudeLiquid hydrogen and aluminum trimethyl as highly reactive chemical additives in turbojet afterburner to promote fuel combustion process
Document ID
19650014455
Document Type
Other - NACA Research Memorandum
Authors
Sivo, J. N. (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
September 30, 1958
Subject Category
Propulsion Systems
Report/Patent Number
NACA-RM-E58G10
Accession Number
65N24056
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID HYDROGEN
FUEL COMBUSTION
TURBOJET ENGINE
ADDITIVE
AFTERBURNER
ALUMINUM COMPOUND

Related Records

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