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Design definition study of a NASA/Navy lift/cruise fan technology V/STOL airplane: Risk assessment addendum to the final reportAn assessment of risk, in terms of delivery delays, cost overrun, and performance achievement, associated with the V/STOL technology airplane is presented. The risk is discussed in terms of weight, structure, aerodynamics, propulsion, mechanical drive, and flight controls. The analysis ensures that risks associated with the design and development of the airplane will be eliminated in the course of the program and a useful technology airplane that meets the predicted cost, schedule, and performance can be produced.
Document ID
19760011012
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zabinsky, J. M.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Burnham, R. W.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Flora, C. C.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Gotlieb, P.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Grande, D. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Gunnarson, D. W.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Howard, W. M.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Hunt, D.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Jakubowski, G. W.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Johnson, P. E.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-137729
D6-42611-ADD
Report Number: NASA-CR-137729
Report Number: D6-42611-ADD
Accession Number
76N18100
Funding Number(s)
CONTRACT_GRANT: NAS2-6563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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