Airbreathing space launcher interest of a fully variable geometry propulsion system

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Bouchez, Marc ^a   Levine, Vadim ^b   Falempin, François ^c   Davidenko, Dmitri ^b   Avrashkov, Valery ^b  

^a AEROSPATIALE MATRA Missiles   (France)

^b MOSCOW AVIATION INSTITUTE NATIONAL RESEARCH UNIVERSITY   (Russian Federation)

^c ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BUDGET CONTROL; COMBUSTORS; COMPUTER SOFTWARE REUSABILITY; DUAL FUEL ENGINES; ECONOMIC AND SOCIAL EFFECTS; ENGINES; FIGHTER AIRCRAFT; GEARS; GEOMETRY; LANDING GEAR (AIRCRAFT); PROPULSION; ROCKETS; SPACECRAFT PROPULSION; VEHICLE PERFORMANCE; VEHICLES;

AIR BREATHING ENGINES; AIR-BREATHING PROPULSION; DEVELOPMENT AND OPERATIONS; FIXED COMBUSTOR GEOMETRY; HYPERSONIC PROPULSION; LARGE-SCALE PROTOTYPE; RESEARCH AND TECHNOLOGY PROGRAMS; TECHNOLOGY DEVELOPMENT;

MACH NUMBER;

EID: 84963864683     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (23)

1. F. Falempin, D. Scherrer, G. Laruelle, Ph. Rostand, G. Fratacci, J.L. Schultz French hypersonic propulsion program PREPHA-results, lessons & perspectives AIAA-98-1565-Norfolk
2. F. Falempin PREPHA Program-System studies synthesis XIIIISABE-Chattanooga – 1997
3. A. Chevalier, V. Levine, M. Bouchez, D. Davidenko French-Russian Partnership on Hypersonic Wide Range Ramjets AIAA-96-4554
4. S. Baranovsky, I. Gilevitch, D. Davidenko, K. Kanin, A. Stukov, A. Tikhonov A Program of the Scramjet Design and Optimization AIAA 91-5073
5. V.N. Avrashkov, S. Baranovsky, V.M. Levin Gasdynamic features of Supersonic Kerosene Combustion in a Model Combustion Chamber AIAA 90-5268
6. S.I. Baranovsky, V.M. Levin, A.S. Nadvorsky, A.I. Turishev Heat transfer in supersonic Coaxial Reacting Jets Int. J. Heat Mass Transfer, Vol. 33, N°4, 1990, pp. 641-648
7. V.M. Levin, Gasdynamics of flow structure in a channel under thermal and mechanical throttling, 1 st Int. Symposium on Experimental and Computational Aerodynamics of internal Flows, July 8-12, 1990, Beijing, China.
8. S. Baranovsky, D. Davidenko, I.V. Konovalov, V.M. Levin Experimental Study of the hydrogen supersonic combustion. 9th World hydrogen Energy Conf., 22-25 June, 1992, Paris
9. S. Baranovsky, D. Davidenko, V. Levin Test facility for the flow structure study in the supersonic combustion chamber 6th Int. Symposium on Flow vizualization, 5-9 October, 1992, Yokohama, Japan
10. S. Baranovsky, V.M. Levin Wide Range Combustion Chamber of Ramjet AIA A-91-5094
11. Alain Chevalier, Marc Bouchez, Dominique Bouchaud, Isabelle Auneau, Nicole Montmayeur An industrial point of view on scramjet combustor design. IUTAM symposium, Poitiers, October 1995
12. A. Wagner et al., Integration of a Combined Engine Propulsion System into a SSTO launcher, 1995, AIAA-95-6044
13. I. Auneau, P. Garnero, P. Duveau, Design and Optimization Methods for Scramjet Inlets, 1995, AIAA-95-6017
14. M. Bouchez et al. Scramjet combustor design in France, AIAA 95-6094.
15. A. Chevalier, F. Falempin, Review of New French Facilities for PREPHA Program. 1995, AIAA 95-6128
16. A. Chevalier, D. Piton, An original concept of hypersonic facilities: the Adiabatic Compression Wind Tunnel (A.C.W.T.), ESA/ESTEC, 11/94
17. F. Falempin, B. Forrat, J. Baldeck, E. Hermant, 1992, Flight test vehicles, a mandatory step in scramjet development, AIAA-92-5052
18. D. Bouchaud, D. Fournet, P. Herve Temperature and concentration Measurements in a hydrogen-Air Scramjet AIAA 96-4583.
19. Study of a Generic SSTO Vehicle Using Airbreathing Propulsion T. BONNEFOND, F. FALEMPIN, P. VIALA AIAA-96-4490-CP
20. P. Peres, J. Lansalot, M. Bouchez, E. Saunier Advanced Carbon-carbon Injection Strut for Actual Scramjet AIAA 96-4567
21. C. Rothmund, D. Scherrer, M. Bouchez Propulsion System for Airbeathing Launcher in the French Prepha Program AIAA-96-4498, Norfolk, November 18-22, 1996
22. T.M. Atammanchuk, JP. Sislian, R. Dudebout An Aerospace Plane as a Detonation Wave Ramjet/Airframe Integrated Waverider AIAA 95-5022
23. G.P. Menees, H.G. Adehnan, J.L. Cambier, J.V. Bowles Wave Combustors for Trans-Atmospheric Vehicles Journal of Propulsion and Power, Vol. 8, N 3, 1992, pp. 709-713