The French LEA flight test program - Status in 2008

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2008, Pages

  Falempin, Francois ^a,c   Serre, Laurent ^b,c  

^a MBDA FRANCE   (France)

^b ONERA   (France)

^c Aerodynamics   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIR BREATHING PROPULSIONS; AUTONOMOUS FLIGHT; DESIGN GUIDELINES; DETAILED DESIGN; EXPERIMENTAL VEHICLE; FLIGHT TEST; FLIGHT TEST PROGRAMS; FREE JETS; FUEL-COOLED; GROUND TEST FACILITIES; GROUND TESTS; KEYPOINTS; LARGE PARTS; LOW WEIGHT; MECHANICAL STRENGTH; NUMERICAL SIMULATION; OPERATIONAL APPLICATIONS; PRELIMINARY DESIGN REVIEWS; PROPULSION SYSTEM; REASONABLE ACCURACY; SCIENTIFIC PROGRAMS; STEP-BY-STEP; TECHNOLOGICAL PROGRAMS; TECHNOLOGY DEVELOPMENT; THERMAL ANALYSIS; VARIABLE GEOMETRY;

COMBUSTION; COMBUSTION CHAMBERS; COMPUTER SIMULATION; DESIGN; DRAG; FLIGHT SIMULATORS; FUELS; HYPERSONIC AERODYNAMICS; MACH NUMBER; SPACECRAFT PROPULSION; TECHNOLOGICAL FORECASTING; TECHNOLOGY; TESTING; THERMOANALYSIS; UNMANNED AERIAL VEHICLES (UAV); VEHICLES;

HYPERSONIC VEHICLES;

EID: 77958453947     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (39)

1. F. FALEMPIN, Ramjet/Scramjet technology - French capabilities - AIAA - 99-2377-Los Angeles
2. F. FALEMPIN, Ph. NOVELLI, P. HENDRICK, A. SOUCHIER, Airbreathing/rocket combined cycle propulsion efforts in Europe, AAAF - 2002-268 - Versailles
3. Ph. NOVELLI, W. KOSCHEL, JAPHAR : a joint ONERA-DLR research project for high-speed airbreathing propulsion, XIV ISABE - Florence - IS 7091-1999
4. Ph. NOVELLI, Progress of the JAPHAR cooperation between ONERA and DLR on hypersonic airbreathing prop. - AIAA-2001--Kyoto
5. Th. EGGERS, Ph. NOVELLI, Design studies for a M 8 dual mode ramjet flight test vehicle - AIAA - 99-4877
6. M. BOUCHEZ, F. FALEMPIN, V. LEVINE, V. AVRASHKOV, D. DAVIDENKO, French-Russian partnership on hypersonic Wide Range Ramjet: status in 2001, AIAA-2001-1872
7. M. BOUCHEZ, J-P. MINARD, V. LEVINE, V. AVRASHKOV, D. DAVIDENKO, French-Russian partnership on hypersonic Wide Range Ramjet: status in 2002, AIAA-2002-5254
8. M. BOUCHEZ, V. LEVINE, V. AVRASHKOV, French-Russian Cooperation on Dual-Mode Ramjet : significant step passed for technology and combustion processes mastering, AIAA-2003-7004.
9. L. SERRE, F. FALEMPIN, Promethee:The French Military Hypersonic Propulsion Program, AIAA-2003-6950
10. C. BOUQUET, J. THEBAULT, P.SOYRIS, R. FISCHER, Fully ceramic composite heat exchanger qualification for advanced combustion chambers, AIAA-2005-3433
11. F. FALEMPIN, M. GOLDFELD, R. NESTOULIA, A.STAROV, Evaluation of a variable geometry inlet for dual mode ramjet - AIAA-2002-5232 - Orléans
12. J-P. MINARD, RAPIERE:Innovative industrial optical measurement system for scramjet flows, AIAA-2002-5156
13. M. GOLDFELD, R. NESTOULIA, F. FALEMPIN, Direct measurement of friction in the boundary layer at supersonic flow velocities, AIAA-2002-5199-Orléans
14. M. SICARD, F. SER, B. RAEPSAET, C. MASSON, Kinetic study and decomposition products determination of a N-Alkane endothermic fuel, AIAA - 2005-3402
15. E. DANIAU,M. BOUCHEZ,O. HERBINET,P. MARQUAIRE,F. BATTIN-LECLERC,R. FOURNET, R. BOUNACEUR, Fuel reforming for scramjet thermal management and combustion optimization, AIAA-2005-3403
16. E. DANIAU, M. SICARD, Experimental and numerical investigations of an endothermic fuel cooling capacity AIAA - 2005-3404
17. M.BOUCHEZ, E.DANIAU, N.GASCOIN,P.GILLARD, S.BERNARD, G.ABRAHAM, Y.TOURE, Measurements for fuel reforming for scramjet thermal management and combustion optimization : status of the COMPARER project, AIAA - 2006 - Canberra
18. M.BOUCHEZ, E.SAUNIER, P. PERES, J.LANSALOT, Advanced carbon/carbon injection strut for actual scramjet, AIAA - 96-4567
19. M. BOUCHEZ, E. DUFOUR, E. DANIAU, Semi-empirical and CFD analysis of actively cooled dual-mode ramjets : 2006 status, AIAA - 2006-8073
20. nd EUCASS - 2007-Brussels - paper no 308
21. M. BOUCHEZ, S. BEYER, PTAH-SOCAR Fuel-cooled Composite Materials Structure, AIAA-2008-2626
22. JP. MINARD, F. FALEMPIN, METHYLE : a long endurance test facility for dual-mode ramjet combustor technologies, AIAA-2008-2650
23. M. BOUCHEZ, E. DANIAU, N. VISEZ, O. HERBINET, PM. MARQUAIRE, Hydrocarbons heterogeneous pyrolisis : experiments and modeling for scramjet thermal management, AIAA-2008-XXXX
24. M. SICARD, XXXX, AIAA-2008-XXXX
25. D. DAVIDENKO, I. GOKALP, E. DUFOUR, D. GAFFIE, Kinetic mechanism validation and numerical simulations of supersonic combustion of methane-hydrogen fuel, AIAA - 2002-5207-Orléans
26. D. DAVIDENKO, I. GOKALP, E. DUFOUR, D. GAFFIE, Numerical simulation of supersonic combustion of methane-hydrogen fuel in an experimental combustion chamber Moscow - July 2003
27. D. DAVIDENKO, I. GOKALP, E. DUFOUR, Numerical modelling of inert and reacting compressible turbulent jets, AIAA - 2005-3237
28. D.DAVIDENKO, I. GOKALP, E. DUFOUR, Ph. MAGRE, Systematic study of the supersonic combustion in an experimental combustion chamber, AIAA - 2006 - Canberra
29. O.DESSORNES, M. BOUCHEZ, Combustion experiments of liquid kerosene and H2/CH4 mixing in a dualmode ramjet, AIAA-2005-3400
30. M. BOUCHEZ, D. SCHERRER, Combustion investigation for dual-mode ramjet for the LEA program, AIAA-2008-2648
31. L. SERRE, F. FALEMPIN, Development of a Free Jet Test Facility for the French LEA flight test program, AIAA-2008-2651
32. F. FALEMPIN, French hypersonic program PREPHA - System studies synthesis, XIII ISABE - 1997
33. F. FALEMPIN, M. BOUCHEZ, L. SERRE, C. BRUNO, P. HENDRICK, Airbreathing Propulsion for Future Space Launchers - Proposal for a Minimum R&T Program for Europe, AIAA - 2005-3362 - Capua
34. F. FALEMPIN, L. SERRE, LEA flight test program - Status in 2006, AIAA - 2006-7925
35. nd EUCASS - 2007-Brussels - paper no420
36. Papier ONERA ? (par exemple AIAA Capua)
37. F.FALEMPIN, M. BOUCHEZ, M. CALABRO, Preliminary design of a fully axisymmetric airbreathing micro space launcher, AIAA-2008-2641
38. F. FALEMPIN, E. DANIAU, A Contribution to the Development of Actual Continuous Detonation Wave Engines, AIAA-2008-2679
39. th AIAA international space planes and hypersonic systems and technologies - 2008-Dayton (OH)