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Volumn , Issue , 1999, Pages

Airbreathing Space launcher interest of a fully variable geometry propulsion system-status 1999

Author keywords

[No Author keywords available]

Indexed keywords

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

EID: 84963859113     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (2)

References (25)
  • 9
    • 84895970222 scopus 로고
    • Test facility for the flow structure study in the supersonic combustion chamber
    • 5-9 october, Yokohama, Japan
    • 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
    • (1992) 6Th Int. Symposium on Flow Vizualization
    • Baranovsky, S.1    Davidenko, D.2    Levin, V.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.