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Volumn , Issue , 1996, Pages

French-russian partnership on hypersonic wide range ramjets

Author keywords

[No Author keywords available]

Indexed keywords

AIR INTAKES; COMBUSTION; ENGINES; LAUNCHING; PROPULSION; SPACECRAFT; SUPERSONIC AIRCRAFT; TECHNOLOGY TRANSFER;

EID: 84983210811     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (22)
  • 7
    • 84983111214 scopus 로고    scopus 로고
    • Wide Range Combustion Chamber of Ramjet AIAA-91-5094
    • S. Baranovsky, V. M. Levin Wide Range Combustion Chamber of Ramjet AIAA-91-5094
    • Baranovsky, S.1    Levin, V.M.2
  • 8
    • 84983154889 scopus 로고    scopus 로고
    • Future Launch Vehicles at AEROSPATIALE: A Survey, AIAA-93-5051
    • A. Wagner, R. Thevenot, Future Launch Vehicles at AEROSPATIALE: A Survey, AIAA-93-5051
    • Wagner, A.1    Thevenot, R.2
  • 9
    • 84983132877 scopus 로고    scopus 로고
    • Integration of a Combined Engine Propulsion System into a SSTO launcher, 1995, AIAA-95-6044
    • A. Wagner et al., Integration of a Combined Engine Propulsion System into a SSTO launcher, 1995, AIAA-95-6044
    • Wagner, A.1
  • 13
    • 84983109706 scopus 로고    scopus 로고
    • Propulsion System for Airbeathing Launcher in the French Prepha Program AIAA-96-4498, Norfolk, November 18-22
    • C. Rothmund, D. Schemer, M. Bouchez, Propulsion System for Airbeathing Launcher in the French Prepha Program AIAA-96-4498, Norfolk, November 18-22, 1996
    • (1996)
    • Rothmund, C.1    Schemer, D.2    Bouchez, M.3
  • 14
    • 84983170690 scopus 로고    scopus 로고
    • An original concept of hypersonic facilities: the Adiabatic Compression Wind Tunnel (A. C. W. T.), ESNESTEC, 11/94
    • A. Chevalier, D. Piton, An original concept of hypersonic facilities: the Adiabatic Compression Wind Tunnel (A. C. W. T.), ESNESTEC, 11/94
    • Chevalier, A.1    Piton, D.2
  • 15
    • 84983211240 scopus 로고
    • Flight test vehicles, a mandatory step in scramjet development, AIAA-92-5052
    • F. Falempin, B. Forrat, J. Baldeck, E. Hermant, 1992, Flight test vehicles, a mandatory step in scramjet development, AIAA-92-5052
    • (1992)
    • Falempin, F.1    Forrat, B.2    Baldeck, J.3    Hermant, E.4
  • 16
    • 84983105260 scopus 로고    scopus 로고
    • Advanced-To-Orbit Propulsion concepts AIAA-86-1386
    • C. J. O’Brien and A. C. Kobayashi, Advanced-To-Orbit Propulsion concepts AIAA-86-1386
    • O, C.J.1    ’Brienkobayashi, A.C.2
  • 17
    • 84983169302 scopus 로고    scopus 로고
    • Scramjet combustor design in France, AlAA 95-6094
    • M. Bouchez et al., Scramjet combustor design in France, AlAA 95-6094.
    • Bouchez, M.1
  • 18
    • 84983109721 scopus 로고    scopus 로고
    • Temperature and concentration Measurements in a hydrogen-Air Scramjet AlAA 96-4583
    • D. Bouchaud, D. Fournet, P. Hervé, Temperature and concentration Measurements in a hydrogen-Air Scramjet AlAA 96-4583.
    • Bouchaud, D.1    Fournet, D.2    Hervé, P.3
  • 21
    • 84983210519 scopus 로고    scopus 로고
    • An Aerospace Plane as a Detonation Wave Ramje/Airframe Integrated Waverider AlAA 95-5022
    • T. M. Atammanchuk, JP. Sislian, R. Dudebout An Aerospace Plane as a Detonation Wave Ramje/Airframe Integrated Waverider AlAA 95-5022
    • Atammanchuk, T.M.1    Sislian, J.P.2    Dudebout, R.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.