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Hyper-X Engine Testing in the NASA Langley 8-Foot High Temperature TunnelAirframe-integrated scramjet engine tests have been completed at Mach 7 in the NASA Langley 8-Foot High Temperature Tunnel under the Hyper-X program. These tests provided critical engine data as well as design and database verification for the Mach 7 flight tests of the Hyper-X research vehicle (X-43), which will provide the first-ever airframe-integrated scramjet flight data. The first model tested was the Hyper-X Engine Model (HXEM), and the second was the Hyper-X Flight Engine (HXFE). The HXEM, a partial-width, full-height engine that is mounted on an airframe structure to simulate the forebody features of the X-43, was tested to provide data linking flowpath development databases to the complete airframe-integrated three-dimensional flight configuration, and to isolate effects of ground testing conditions and techniques. The HXFE, an exact geometric representation of the X-43 scramjet engine mounted on an airframe structure that duplicates the entire three-dimensional propulsion flowpath from the vehicle leading edge to the vehicle base, was tested to verify the complete design as it will be flight tested. This paper presents an overview of these two tests, their importance to the Hyper-X program, and the significance of their contribution to scramjet database development.
Document ID
20010011859
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Huebner, Lawrence D.
(NASA Langley Research Center Hampton, VA United States)
Rock, Kenneth E.
(NASA Langley Research Center Hampton, VA United States)
Witte, David W.
(NASA Langley Research Center Hampton, VA United States)
Ruf, Edward G.
(NASA Langley Research Center Hampton, VA United States)
Andrews, Earl H., Jr.
(FDC/NYMA, Inc. Hampton, VA United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2000
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2000-3605
Meeting Information
Meeting: Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: July 17, 2000
End Date: July 19, 2000
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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