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NASA N+3 Subsonic Fixed Wing Silent Efficient Low-Emissions Commercial Transport (SELECT) Vehicle StudyA conceptual commercial passenger transport study was performed to define a single vehicle for entry into service in the 2030 to 2035 timeframe, meeting customer demands as well as NASA goals for improved fuel economy, NOx emissions, noise, and operability into smaller airports. A study of future market and operational scenarios was used to guide the design of an advanced tube-and-wing configuration that utilized advanced material and structural concepts, an advanced three-shaft high-bypass turbofan engine, natural laminar flow technology, and a suite of other advanced technologies. This configuration was found to meet the goals for NOx emissions, noise, and field length. A 64 percent improvement in fuel economy compared to a current state-of-the-art airliner was achieved, which fell slightly short of the desired 70 percent goal. Technology maturation plans for the technologies used in the design were developed to help guide future research and development activities.
Document ID
20100042399
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Bruner, Sam
(Northrop Grumman Corp. El Segundo, CA, United States)
Baber, Scott
(Northrop Grumman Corp. El Segundo, CA, United States)
Harris,Chris
(Northrop Grumman Corp. El Segundo, CA, United States)
Caldwell, Nicholas
(Northrop Grumman Corp. El Segundo, CA, United States)
Keding, Peter
(Northrop Grumman Corp. El Segundo, CA, United States)
Rahrig, Kyle
(Northrop Grumman Corp. El Segundo, CA, United States)
Pho, Luck
(Northrop Grumman Corp. El Segundo, CA, United States)
Wlezian, Richard
(Tufts Univ. Medford, MA, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2010
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/CR-2010-216798/REVA
E-17429
Funding Number(s)
WBS: WBS 561581.02.08.03.13.66
CONTRACT_GRANT: NNC08CA86C
Distribution Limits
Public
Copyright
Public Use Permitted.
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