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Energy efficient engine. Volume 1: Component development and integration programTechnology for achieving lower installed fuel consumption and lower operating costs in future commercial turbofan engines are developed, evaluated, and demonstrated. The four program objectives are: (1) propulsion system analysis; (2) component analysis, design, and development; (3) core design, fabrication, and test; and (4) integrated core/low spoon design, fabrication, and test.
Document ID
19850002684
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
October 30, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5594-179-VOL-1
NASA-CR-173084
SASR-7-VOL-1
NAS 1.26:173084
Report Number: PWA-5594-179-VOL-1
Report Number: NASA-CR-173084
Report Number: SASR-7-VOL-1
Report Number: NAS 1.26:173084
Accession Number
85N10992
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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