Abstract
The potential short-supply of petroleum-based fuels has led to activities by NASA to establish technical characteristics of air transportation systems that would use hydrogen-fueled aircraft. These activities cover sources and production of liquid hydrogen,1 aircraft configurations,2 and air terminal modifications, as affected by the introduction of liquid-hydrogen-fueled aircraft.3,4
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References
R.D. Witcofski, Alternate Aircraft Fuels PROSPECTS and Operational Implications, NASA TMS 74036 (May 1977).
G.D. Brewer, R.E. Morris, R.H. Lange, and J.W. Moore, Study of the Application of Hydrogen Fuel to Long-Range Subsonic Transport Aircraft, NASA CR-132559 (January 1975).
G.D. Brewer, LH2 Airport Requirements Study, NASA CR-2700 (March 1976).
Anon, An Exploratory Study to Determine the Integrated Technological Air Transportation System Ground Requirements of Liquid-Hydrogen-Fueled Subsonic, Long-Haul Civil Air Transports, NASA CR-2699 (May 1976).
R.G. Helenbrook and J.Z. Colt, Development and Validation of Purged Thermal Protection Systems for Liquid Hydrogen Fuel Tanks of Hypersonic Vehicles, NASA CR-2829 (June 1977).
R.R. Dixon, L.E. Edelman, and D.E. McLain, “Effect of Aging in Thermal Conductivity of Cellular Materials,” Journal of Cellular Plastics (Jan.-Feb. 1970 ), p. 44.
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© 1979 Plenum Press, New York
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Sharpe, E.L., Helenbrook, R.G. (1979). Durability of Foam Insulation for LH2 Fuel Tanks of Future Subsonic Transports. In: Clark, A.F., Reed, R.P., Hartwig, G. (eds) Nonmetallic Materials and Composites at Low Temperatures. Cryogenic Materials Series. Springer, Boston, MA. https://doi.org/10.1007/978-1-4615-7522-1_14
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DOI: https://doi.org/10.1007/978-1-4615-7522-1_14
Publisher Name: Springer, Boston, MA
Print ISBN: 978-1-4615-7524-5
Online ISBN: 978-1-4615-7522-1
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