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Volumn , Issue , 1999, Pages 1-21

An airbreathing launch vehicle design with turbine-based lowspeed propulsion and dual mode scramjet high-speed propulsion

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; DESIGN; LAUNCH VEHICLES; SPACECRAFT; SPACECRAFT PROPULSION; STRUCTURAL FRAMES; TURBINES; VEHICLES;

EID: 84983121554     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (20)

References (9)
  • 3
    • 84983135448 scopus 로고    scopus 로고
    • Version 3.1.2, TechnoSoft, Inc. Cincinnati, OH. Copyright
    • Adaptive Modeling Language, Version 3.1.2, TechnoSoft, Inc. Cincinnati, OH. Copyright 1999.
    • (1999) Adaptive Modeling Language
  • 4
    • 84983105548 scopus 로고
    • Release 9839, Version 20, Parametric Technology Corporation, Waltham, MA, Copyright
    • Pro/ENGINEER, Release 9839, Version 20, Parametric Technology Corporation, Waltham, MA, Copyright 1988-1998.
    • (1988) Pro/ENGINEER
  • 6
    • 0004732485 scopus 로고    scopus 로고
    • North American Aircraft Operations, RockwelMnternational, Los Angeles, CA
    • Sova, G., Divan, P., "Aerodynamic Preliminary System II," North American Aircraft Operations, RockwelMnternational, Los Angeles, CA.
    • Aerodynamic Preliminary System II
    • Sova, G.1    Divan, P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.