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LCX: Proposal for a low-cost commercial transportThe LCX has been developed in response to a request for proposal for an aircraft with 153 passenger capacity and a range of 3000 nautical miles. The goals of the LCX are to provide an aircraft which will achieve the stated mission requirements at the lowest cost possible, both for the manufacturer and the operator. Low cost in this request is defined as short and long term profitability. To achieve this objective, modern technologies attributing to low-cost operation without greatly increasing the cost of manufacturing were employed. These technologies include hybrid laminar flow control and the use of developing new manufacturing processes and philosophies. The LCX will provide a competitive alternative to the use of the Airbus A319/320/321 and the Boeing 737 series of aircraft. The LCX has a maximum weight of 150,000 lb. carried by a wing of 1140 ft(exp 2) and an aspect ratio of 10. The selling price of the LCX is 31 million in 1994 US dollars.
Document ID
19950006232
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hartman, Troy
(Universities Space Research Association Columbia, MD, United States)
Hayatdavoudi, Maziar
(Universities Space Research Association Columbia, MD, United States)
Hettinga, Joel
(Universities Space Research Association Columbia, MD, United States)
Hooper, Matt
(Universities Space Research Association Columbia, MD, United States)
Nguyen, Phong
(Universities Space Research Association Columbia, MD, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-197186
NAS 1.26:197186
Report Number: NASA-CR-197186
Report Number: NAS 1.26:197186
Accession Number
95N12645
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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