로켓기반 공기흡입추진 엔진이 적용된 재사용 발사체의 요구 성능 및 중량 분석

' 로켓기반 공기흡입추진 엔진이 적용된 재사용 발사체의 요구 성능 및 중량 분석' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • ramjet(램제트)
  • reusable launch vehicle(재사용 발사체)
  • rocket-based combined cycle(로켓 기반 복합 사이클)
  • scramjet(스크램 제트)
  • specific impulse(비추력)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
77 0

0.0%

' 로켓기반 공기흡입추진 엔진이 적용된 재사용 발사체의 요구 성능 및 중량 분석' 의 참고문헌

  • Scramjet Engines Enabling the Seamless Integration of Air & Space Operation, Pratt & Whitney Space Propulsion, Hypersonics
    Andreadis, D. West Palm Beach [2004]
  • SCCREAM : A Conceptual Rocket-Based Combined-Cycle Engine Performance Analysis Tool
    Olds, J.R. Journal of Propulsion and Power 17 (2) : 333 ~ 339 [2001]
  • Results of a Rocket-Based Combined-Cycle SSTO Design Using Parametric MDO Methods
    Olds, J.R. SAE-941165 [1994]
  • RBCC엔진을 적용한 재사용발사체의 중량저감효과
    강상훈 한국추진공학회지 17 (3) : 56 ~ 66 [2013]
  • Optimal Control Programs for Airbreathing Propulsion System for Single-Stage-To-Orbit
    Yugov, O. K 40th IAF Congress [1989]
  • Multidisciplinary Design Techniques Applied to Conceptual Aerospace Vehicle Design
    Olds, J.R. NASA-CR-194409 [1993]
  • Hypersonic Intake Starting Characteristics-A CFD Validation Study
    Saha, S. Defence Science Journal 62 (3) : 147 ~ 152 [2012]
  • Design of Sub-scale Rocket-Ramjet Combined Cycle Engine Model
    Kanda, T. 56th International Astronautical Congress [2005]
  • Conceptual Study of a Two-Stage Air-Breading Reusable Launch Vehicle
    Takahashi, S. Journal of Spacecraft and Rockets 34 (5) : 628 ~ 635 [1997]
  • Conceptual Design of Rocket Based Combined Cycle Engine
    Lee, Y. J. 33th KSPE Fall Conference : 581 ~ 585 [2009]
  • Conceptual Design of Flight Demonstrator Vehicles for the ATREX Engine
    Mizobata, K. 12th AIAA International Space Planes and Hypersonic Systems and Technologies [2003]