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• W2044252656 abstract "Wide Range Ramjets appear to be a good solution for propulsion of reusable space launchers. These airbreathing engines are able to work from Mach 2 to 6 with subsonic combustion and then with supersonic combustion from Mach 6 to Mach 12 (for example). It could be interesting to complete the Wide Range Ramjet operation with detonationbased cycles. AEROSPATIALE has now a good experience of actual size hydrogen fueled hypersonic ramjets, from the system point of view, the air intake design, the combustors tested in Bourges up to Mach 6,5, the CFD support, the testing and measurement technics (ground and flight test methodology) and the engine structural point of view, with close connection with the launcher designer. The intest CHAMOIS supersonic combustion ramjet is an example of this know-how. Moscow Aviation Institute (M .A. I .) propulsion specialists have been working since the sixties on hypersonic ramjets and scramjets. A lot of experiments have been performed, and the laboratory's engineers have an accurate understanding (including high level of mathematical modelization) of the phenomena occuring in such engines. The interactions with the air intake, the nozzle and the vehicle have also been taken into account. The M.A.I. materials laboratory has been associated to design, build and test the structures required for these engines. Three years of personal contacts and high level of cooperation have shown that the AEROSPATIALE and Moscow Aviation Institute multicomponent methodologies for hypersonic propulsion are similar but complementary. The main common features are the both analytical and experimental understanding, the systematic experimental validation of the thermodynamic and structural options for the engine, the interest on the Wide Range Ramjet for reusable space launchers. Copyright 1996 by AEROSPATIALE and Moscow Aviation Institute. Published by the American Institute of Aeronautics and Astronautics, Inc with permission. The use of kerosen and then hydrogen on the trajectory, the study of integration of detonation-based cycle to the Wide Range Ramjet, the solutions for the movable parts are particulary studied in this cooperation. The test methodology and in particular the scale effect between the full scale space launcher, a 30 meter medium vehicle and a small Flying Test Bed, are also under common study." @default.
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• W2044252656 date "2001-11-01" @default.
• W2044252656 modified "2023-09-25" @default.
• W2044252656 title "French-Russian Partnership on Hypersonic Wide-Range Ramjets" @default.
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• W2044252656 doi "https://doi.org/10.2514/2.5892" @default.
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