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Experimental Investigation of an Integrated Strut-Rocket/Scramjet Operating at Mach 4.0 and 6.5 ConditionsA series of tests were conducted to investigate RBCC performance at ramjet and scramjet conditions. The hardware consisted of a linear strut-rocket manufactured by Aerojet and a dual-mods scramjet combustor. The hardware was tested at NASA Langley Research Center in the Direct Connect Supersonic Combustion Test Facility at Mach 4.0 and 6.5 simulated flight conditions.
Document ID
19980237004
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Hawk, Clark (Alabama Univ. Huntsville, AL United States)
Nelson, Karl (Alabama Univ. Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Joint Propulsion Meeting
Location: Cleveland, OH
Country: United States
Start Date: July 15, 1998
End Date: July 17, 1998
Sponsors: Department of the Navy, NASA Headquarters, Department of the Air Force, Department of the Army
Funding Number(s)
CONTRACT_GRANT: NGT-51371
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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