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The Design and Testing of a Miniature Turbofan EngineOff-the-shelf jet propulsion in the 50 - 500 lb thrust class sparse. A true twin-spool turbofan in this range does not exist. Adapting an off-the-shelf turboshaft engine is feasible. However the approx.10 Hp SPT5 can t quite make 50 lbs. of thrust. Packaging and integration is challenging, especially the exhaust. Building on our engine using a 25 Hp turboshaft seems promising if the engine becomes available. Test techniques used, though low cost, adequate for the purpose.
Document ID
20090040469
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Cosentino, Gary B.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Murray, James E.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 24, 2013
Publication Date
November 10, 2009
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
09ATC-0241
DFRC-1074
Meeting Information
Meeting: SAE 2009 Aerotech Congress and Exhibition
Location: Seattle, WA
Country: United States
Start Date: November 10, 2009
End Date: November 12, 2009
Sponsors: Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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