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The General Aviation Propulsion (GAP) ProgramThe General Aviation Propulsion (GAP) Program Turbine Engine Element focused on the development of an advanced small turbofan engine. Goals were good fuel consumption and thrust-to-weight ratio, and very low production cost. The resulting FJX-2 turbofan engine showed the potential to meet all of these goals. The development of the engine was carried through to proof of concept testing of a complete engine system. The proof of concept engine was ground tested at sea level and in altitude test chambers. A turboprop derivative was also sea-level tested.
Document ID
20080031112
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Date Acquired
August 24, 2013
Publication Date
July 1, 2008
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2008-215266
E-16536
Funding Number(s)
WBS: WBS 984754.02.07.03.11.02
CONTRACT_GRANT: NCC3-514
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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