Airbreathing space launcher interest of a fully variable geometry propulsion system and corresponding French-Russian partnership

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Bouchez, Marc ^a   Levine, Vadim ^b   Davidenko, Dmitri ^b   Avrashkov, Valery ^b   Genevieve, Pascal ^a  

^a AEROSPATIALE MATRA Missiles   (France)

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

Author keywords

[No Author keywords available]

Indexed keywords

AVIATION; COMPUTER SOFTWARE REUSABILITY; ENGINES; GEARS; GEOMETRY; HYPERSONIC VEHICLES; LANDING GEAR (AIRCRAFT); MISSILES; RAMJET ENGINES; ROCKETS; TAKEOFF; TECHNOLOGY; VEHICLES;

AIR-BREATHING PROPULSION; EXPERIMENTAL VEHICLE; HYPERSONIC PROPULSION; INCREMENTAL DEVELOPMENT; JOINT PROPULSION CONFERENCES; LARGE-SCALE PROTOTYPE; RESEARCH AND TECHNOLOGY PROGRAMS; TECHNOLOGY DEVELOPMENT;

SPACECRAFT PROPULSION;

EID: 84873275410     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (31)

1. F. Falempin, D. Scherrer, G. Larueile, 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. Gileviteh, D. Davidenko, JC. 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, 1st 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 visualization, 5-9 October, 1992, Yokohama, Japan
10. S. Baranovsky, V. M. Levin, Wide Range Combustion Chamber of Ramjet, AIAA-91-5094
11. Alain Chevalier, Marc Bouchez, Dominique Bouehaud, 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. Gamero, 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, L Serre, The Promethee Program-Status in 2000, AIAA-2000-3341, Huntsville, Joint Propulsion Conference, June 2000
18. D. Bouchaud, D. Fournet, P. Herve, Temperature and concentration Measurements in a hydrogen-Air Scramjet, AIAA 96-4583.
19. T. Bonnefon, F. Falempin, P. Viala: Study of a Generic SSTO Vehicle Using Airbreathing Propulsion, A1AA-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 Airbreathing Launcher in the French Prepha Program, AIAA-96-4498, Norfolk, November 8-22, 1996
22. F. Falempin, Fuel-Cooled Composite Materials Structures-Status at Aerospatiale Matra, AIAA-2000-3343, Huntsville, Joint Propulsion Conference, June 2000
23. Marc Bouchez, Vadim Levine, Francis Falempin, Dmitri Davidenko, Valery Avrashkov, Airbreathing space launcher interest of a fully variable geometry propulsion system, AIAA-98-3728, Cleveland, Joint Propulsion Conference, June 1998
24. Marc Bouchez, Vadim Levine, Francois Falempin, Dmitri Davidenko, Valery Avrashkov, Airbreathing space launcher interest of a fully variable geometry propulsion system, AIAA-99-2376, Los Angeles, Joint Propulsion Conference, June 1999
25. J. Olds et al., Hyperion: An SSTO Vision Vehicle Concept Utilizing Rocket-Based Combined Cycle Propulsion, AIAA 99-4944
26. H. Tagushy, M. Maita et al., Airbreather/Rocket combined propulsion system research for Japanese SSTO spaceplane, AIAA 99-4811.
27. DE Pryor, EH Hyde, WJD Escher, Development of a 12-thrust chamber kerosene/oxygen primary rocket subsystem for an early (1964) airaugmented rocket ground test system, AIAA 99-4896
28. F. Falempin et al., MAL'Aerospatiale cooperation on hypersonic Wide Range Ramjet: Evaluation of Thermal Protection System ISABE 99, Florence, September 1999
29. M. Bouchez, High speed propulsion: a ten years Aerospatiale-Matra education contribution, AIAA-99-4894, Norfolk, November 1999
30. S. J. Scotti et al., Active cooling design for scramjet engines using optimization methods, AIAA-88-2265
31. M. Bouchez et al. French-Russian Partnership on Hypersonic Wide Range Ramjet: status in 1999 AIAA-99-4845, Norfolk, Hypersonics Conference, november 1999