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The Edge supersonic transportAs intercontinental business and tourism volumes continue their rapid expansion, the need to reduce travel times becomes increasingly acute. The Edge Supersonic Transport Aircraft is designed to meet this demand by the year 2015. With a maximum range of 5750 nm, a payload of 294 passengers and a cruising speed of M = 2.4, The Edge will cut current international flight durations in half, while maintaining competitive first class, business class, and economy class comfort levels. Moreover, this transport will render a minimal impact upon the environment, and will meet all Federal Aviation Administration Part 36, Stage III noise requirements. The cornerstone of The Edge's superior flight performance is its aerodynamically efficient, dual-configuration design incorporating variable-geometry wingtips. This arrangement combines the benefits of a high aspect ratio wing at takeoff and low cruising speeds with the high performance of an arrow-wing in supersonic cruise. And while the structural weight concerns relating to swinging wingtips are substantial, The Edge looks to ever-advancing material technologies to further increase its viability. Heeding well the lessons of the past, The Edge design holds economic feasibility as its primary focus. Therefore, in addition to its inherently superior aerodynamic performance, The Edge uses a lightweight, largely windowless configuration, relying on a synthetic vision system for outside viewing by both pilot and passengers. Additionally, a fly-by-light flight control system is incorporated to address aircraft supersonic cruise instability. The Edge will be produced at an estimated volume of 400 aircraft and will be offered to airlines in 2015 at $167 million per transport (1992 dollars).
Document ID
19930008866
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Agosta, Roxana
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Bilbija, Dushan
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Deutsch, Marc
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Gallant, David
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Rose, Don
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Shreve, Gene
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Smario, David
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Suffredini, Brian
(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
NAS 1.26:192074
NASA-CR-192074
Report Number: NAS 1.26:192074
Report Number: NASA-CR-192074
Accession Number
93N18055
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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