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Preliminary performance appraisal of Navy V/STOL transport and search-type airplanes using hydrogen fuelFirst-cut estimates are given of the performance advantages of liquid-hydrogen-fueled, ejector wing, V/STOL aircraft designed for shipboard delivery and search-type missions. Results indicate that the use of LH2 could reduce gross weights 30 percent, empty weights 15 percent, and energy consumption 10 percent for a fixed payload and mission. If gross weight is fixed, the delivery range could be increased about 60 percent or the hover time during a search mission doubled. No analysis or discussion of the economic and operational disadvantages is presented.
Document ID
19740018322
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Strack, W. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-71550
E-7962
Report Number: NASA-TM-X-71550
Report Number: E-7962
Accession Number
74N26435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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