NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Definition study for variable cycle engine testbed engine and associated test programThe product/study double bypass variable cycle engine (VCE) was updated to incorporate recent improvements. The effect of these improvements on mission range and noise levels was determined. This engine design was then compared with current existing high-technology core engines in order to define a subscale testbed configuration that simulated many of the critical technology features of the product/study VCE. Detailed preliminary program plans were then developed for the design, fabrication, and static test of the selected testbed engine configuration. These plans included estimated costs and schedules for the detail design, fabrication and test of the testbed engine and the definition of a test program, test plan, schedule, instrumentation, and test stand requirements.
Document ID
19790004877
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vdoviak, J. W.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
R78AEG551
NASA-CR-159459
Report Number: R78AEG551
Report Number: NASA-CR-159459
Accession Number
79N13048
Funding Number(s)
CONTRACT_GRANT: NAS3-20582A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available