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The use of hydrogen for aircraft propulsion in view of the fuel crisisSome factors influencing the technical feasibility of operating a liquid hydrogen-fueled airplane are discussed in light of the projected decrease of fossil fuels. Other sources of energy, such as wind, tidal, solar, and geothermal, are briefly mentioned. In view of projected decreases in available petroleum fuels, interest has been generated in exploiting the potential of liquid hydrogen (LH2) as an aircraft fuel. Cost studies of LH2 production show it to be more expensive than presently used fuels. Regardless of cost considerations, LH2 is viewed as an attractive aircraft fuel because of the potential performance benefits it offers. Accompanying these benefits, however, are many new problems associated with aircraft design and operations; for example, problems related to fuel system design and the handling of LH2 during ground servicing. Some of the factors influencing LH2 fuel tank design, pumping, heat exchange, and flow regulation are discussed.
Document ID
19730016050
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Weiss, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Propellants
Report/Patent Number
E-7490
NASA-TM-X-68242
Report Number: E-7490
Report Number: NASA-TM-X-68242
Meeting Information
Meeting: NASA Res. and Technol. Advisory Comm. on Aeronaut. Operating Systems
Location: Moffett Field, CA
Country: United States
Start Date: March 7, 1973
End Date: March 8, 1973
Accession Number
73N24777
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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