NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Energy efficient engine component development and integration programThe technology that will improve the energy efficiency of propulsion systems for subsonic commercial aircraft is investigated. A reduction of 14.4% in cruise installed sfc (0.572 versus 0.668 for the CF6-50C) and a direct operation cost reduction in excess of the 5% goal is projected. Noise and emissions projections are consistent with the established goals.
Document ID
19830013933
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
January 30, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
R81AEG316
NAS 1.26:170089
SAR-6
NASA-CR-170089
Report Number: R81AEG316
Report Number: NAS 1.26:170089
Report Number: SAR-6
Report Number: NASA-CR-170089
Accession Number
83N22204
Funding Number(s)
CONTRACT_GRANT: NAS3-20643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available