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Phoenix: Preliminary design of a high speed civil transportThe goal of the Phoenix Design Project was to develop a second generation high speed civil transport (HSCT) that will meet the needs of the traveler and airline industry beginning in the 21st century. The primary emphasis of the HSCT is to take advantage of the growing needs of the Pacific Basin and the passengers who are involved in that growth. A passenger load of 150 persons, a mission range of 5150 nautical miles, and a cruise speed of Mach 2.5 constitutes the primary design points of this HSCT. The design concept is made possible with the use of a well designed double delta wing and four mixed flow engines. Passenger comfort, compatibility with existing airport infrastructure, and cost competitive with current subsonic aircraft make the Phoenix a viable aircraft for the future.
Document ID
19930008787
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Aguilar, Joseph
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Davis, Steven
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Jett, Brian
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Ringo, Leslie
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Stob, John
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Wood, Bill
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 9, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-192024
NAS 1.26:192024
Report Number: NASA-CR-192024
Report Number: NAS 1.26:192024
Accession Number
93N17976
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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