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Recent Experimental Results Related to Ejector Mode Studies of Rocket-Based Combined Cycle (RBCC) EnginesContents include the folloving: 1. Motivation. Support NASA's 3d generation launch vehicle technology program. RBCC is promising candidate for 3d generation propulsion system. 2. Approach. Focus on ejector mode p3erformance (Mach 0-3). Perform testing on established flowpath geometry. Use conventional propulsion measurement techniques. Use advanced optical diagnostic techniques to measure local combustion gas properties. 3. Objectives. Gain physical understanding of detailing mixing and combustion phenomena. Establish an experimental data set for CFD code development and validation.
Document ID
20030063014
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Cramer, J. M.
(Pennsylvania State Univ. University Park, PA, United States)
Pal, S.
(Pennsylvania State Univ. University Park, PA, United States)
Marshall, W. M.
(Pennsylvania State Univ. University Park, PA, United States)
Santoro, R. J.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: MSFC Spring Fluids Workshop
Location: Birmingham, AL
Country: United States
Start Date: April 23, 2003
Sponsors: NASA Marshall Space Flight Center
Funding Number(s)
CONTRACT_GRANT: NAS8-40890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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