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THEORETICAL PERFORMANCE OF PROPELLANTS SUITABLE FOR ELECTROTHERMAL JET ENGINESHydrogen, lithium and helium as propellants for electrothermal jet engines
Document ID
19620000290
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jack, J. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
December 1, 1961
Subject Category
Physics, General
Accession Number
62N10290
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LITHIUM
HYDROGEN
ELECTROTHERMAL ENGINE
PROPELLANT
JET ENGINE
JET PROPULSION
HELIUM
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