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COMBINED COMPRESSOR COOLANT INJECTION AND AFTERBURNING FOR TURBOJET THRUST AUGMENTATIONCombined compressor coolant injection and afterburning for turbojet engine thrust augmentation
Document ID
19630002655
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Fenn, D. B. (NASA Lewis Research Center Cleveland, OH, United States)
Huntley, S. C. (NASA Lewis Research Center Cleveland, OH, United States)
Useller, J. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
September 16, 1954
Subject Category
Propellants
Report/Patent Number
NACA-RM-E54G08
Report Number: NACA-RM-E54G08
Accession Number
63N12531
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AFTERBURNING
PROPULSION
TURBINE
INJECTION
COOLANT
TURBOJET ENGINE
COMPRESSOR
THRUST AUGMENTATION

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