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The GE-NASA RTA Hyperburner Design and DevelopmentThe Revolutionary Turbine Accelerator (RTA) project is a ground demonstration of a Mach 4 Turbine Based Combined Cycle engine. This new combined cycle engine developed for the ground-based demonstration will use a new type of augmentor called the hyperburner. The technical features of this new augmenter are introduced in this work. Some of the salient features include a new variable area bypass injector system and a new flame holder configuration. A summary of the hyperburner configuration and the supporting evidence obtained during the hyperburner rig experiments show that hyperburner is a viable burner concept capable of meeting the goals of the RTA ground engine demonstration project.
Document ID
20050196667
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Lee, Jin-Ho
(NASA Glenn Research Center Cleveland, OH, United States)
Winslow, Ralph
(General Electric Aircraft Engines Cincinnati, OH, United States)
Buehrle, Robert J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2005
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-15160
NASA/TM-2005-213803
Meeting Information
Meeting: 40th Combustion, 28th Airbreathing Propulsion, 22nd Propulsion Systems Hazards and 4th Modeling and Simulation Joint Subcommittee Meetings
Location: Charleston, SC
Country: United States
Start Date: June 13, 2005
End Date: June 17, 2005
Sponsors: Department of the Army, NASA Headquarters, Department of the Navy, Department of the Air Force
Funding Number(s)
WBS: WBS 22-065-92-43
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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