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Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liquid oxygen and JP-4 fuel mixture
Document ID
19670022402
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chiccine, B. G. (NASA Lewis Research Center Cleveland, OH, United States)
Shinn, A. M., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Valerino, A. S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-82
Accession Number
67N31731
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JP-4 JET FUEL
JET MIXING
BALLISTIC MISSILE
ROCKET ENGINE
LIQUID OXYGEN /LOX/

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