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Study of aircraft in intraurban transportation systems, volume 3An investigation of three aircraft concepts, deflected slipstream STOL, helicopter VTOL, and fixed wing STOL, is presented. An attempt was made to determine the best concept for the intraurban transportation system. Desirability of the concept was based on ease of maintenance, development timing, reliability, operating costs, and the noise produced. Indications are that the deflected slipstream STOL is best suited for intraurban transportation. Tables and graphs are included.
Document ID
19720003337
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stout, E. G. (Lockheed-California Co. Burbank, CA, United States)
Kesling, P. H. (Lockheed-California Co. Burbank, CA, United States)
Matteson, D. E. (Lockheed-California Co. Burbank, CA, United States)
Sherwood, D. E. (Lockheed-California Co. Burbank, CA, United States)
Tuck, W. R., Jr. (Lockheed-California Co. Burbank, CA, United States)
Vaughn, L. A. (Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1971
Subject Category
General
Report/Patent Number
NASA-CR-114342
Accession Number
72N10986
Funding Number(s)
CONTRACT_GRANT: NAS2-5989
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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