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TBD(exp 3)When asked by the Aeronautical Engineering staff to design a viable supersonic commercial transport, most of the students were well aware that Boeing, McDonnell Douglas, and other aircraft companies had been studying a cadre of transports for more than 30 years and had yet to present a viable aircraft. In the spirit of aviation progress and with much creative license, the TBD design team spearheaded the problem with the full intention of presenting a marketable high speed civil transport in spring of 1992. The project commenced with various studies of future market demands. With the market expansion of American business overseas, the airline industry projects a boom of over 200 million passengers by the year 2000. This will create a much higher demand for time efficient and cost effective inter-continental travel; this is the challenge of the high speed civil transport. The TBD(exp 3), a 269 passenger, long-range civil transport was designed to cruise at Mach 3.0 utilizing technology predicted to be available in 2005. Unlike other contemporary commercial airplane designs, the TBD(exp 3) incorporates a variable geometry wing for optimum performance. This design characteristic enabled the TBD(exp 3) to be efficient in both subsonic and supersonic flight. The TBD(exp 3) was designed to be economically viable for commercial airline purchase, be comfortable for passengers, meet FAR Part 25, and the current FAR 36 Stage 3 noise requirements. The TBD(exp 3) was designed to exhibit a long service life, maximize safety, ease of maintenance, as well as be fully compatible with all current high-traffic density airport facilities.
Document ID
19930008865
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Baughan, Jim
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Calta, David
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Cross, Victor
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Habashi, Mozhi
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Mathias, Donovan
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Northrup, Patti
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-192075
NAS 1.26:192075
Report Number: NASA-CR-192075
Report Number: NAS 1.26:192075
Accession Number
93N18054
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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