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Conceptual design study of 1985 commercial tilt rotor transports. Volume 3: STOL design summaryA conceptual design study is presented of 1,985 commercial tilt rotor STOL transports for a NASA 200 n. mi. (370 km) STOL Mission. A 100-passenger STOL Variant (Bell D313) of the Phase I VTOL Tilt Rotor Aircraft is defined. Aircraft characteristics are given; with the aircraft redesigned to meet 2,000-foot (610 m) field criteria, with emphasis on low fuel consumption and low direct operating cost. The 100-passenger STOL Tilt Rotor Aircraft was analyzed for performance, weights, economics, handling qualities, noise footprint and aeroelastic stability.
Document ID
19760015087
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sambell, K. W.
(Bell Helicopter Co. Fort Worth, TX, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-CR-2690
D313-099-001-VOL-3
Report Number: NASA-CR-2690
Report Number: D313-099-001-VOL-3
Accession Number
76N22175
Funding Number(s)
CONTRACT_GRANT: NAS2-8259
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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