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Design of a spanloader cargo aircraftThe design features of an aircraft capable of fulfilling a long haul, high capacity cargo mission are described. This span-loading aircraft, or flying wing, is capable of carrying extremely large payloads and is expected to be in demand to replace the slow-moving cargo ships currently in use. The spanloader seeks to reduce empty weight by eliminating the aircraft fuselage. Disadvantages are the thickness of the cargo-containing wing, and resulting stability and control problems. The spanloader presented here has a small fuselage, low-aspect ratio wings, winglets, and uses six turbofan engines for propulsion. It will have a payload capacity of 300,000 pounds plus 30 first class passengers and 6 crew members. Its projected market is transportation of freight from Europe and the U.S.A. to countries in the Pacific Basin. Cost estimates support its economic feasibility.
Document ID
19900004900
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Weisshaar, Terrence A.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 6, 2013
Publication Date
June 12, 1989
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-186046
NAS 1.26:186046
Accession Number
90N14216
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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