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Hydrogen-methane fuel control systems for turbojet enginesDesign, development, and test of a fuel conditioning and control system utilizing liquid methane (natural gas) and liquid hydrogen fuels for operation of a J85 jet engine were performed. The experimental program evaluated the stability and response of an engine fuel control employing liquid pumping of cryogenic fuels, gasification of the fuels at supercritical pressure, and gaseous metering and control. Acceptably stable and responsive control of the engine was demonstrated throughout the sea level power range for liquid gas fuel and up to 88 percent engine speed using liquid hydrogen fuel.
Document ID
19740008380
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goldsmith, J. S.
(General Electric Co. Cincinnati, OH, United States)
Bennett, G. W.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-121247
R74AEG153
TM-73-489
Accession Number
74N16493
Funding Number(s)
CONTRACT_GRANT: NAS3-14319
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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