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Some design and operational considerations of a liquid-hydrogen fuel and heat-sink system for turbojet-engine testsLiquid hydrogen used as heat sink for turbine cooling in high temperature turbojet engine
Document ID
19650003106
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Corrington, L. C. (NASA Lewis Research Center Cleveland, OH, United States)
Hennings, G. (NASA Lewis Research Center Cleveland, OH, United States)
Thornbury, K. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 18, 1956
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NACA-RM-E56J18A
Report Number: NACA-RM-E56J18A
Accession Number
65N12707
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBOJET ENGINE
HEAT SINK
HIGH TEMPERATURE ENVIRONMENT
LIQUID HYDROGEN

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