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Altitude performance of a full-scale high-temperature turbojet engine using pentaborane fuel and HEF-2Simulated altitude performance of full scale, high temperature turbojet engine using pentaborane and HEF-2 fuel
Document ID
19670022215
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
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
January 1, 1959
Subject Category
Propulsion Systems
Report/Patent Number
NASA-MEMO-12-31-58E
Report Number: NASA-MEMO-12-31-58E
Accession Number
67N31544
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ALTITUDE SIMULATION
TURBOJET ENGINE
HIGH ENERGY FUEL /HEF/
ENGINE TESTING
PENTABORANE

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