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Volumn , Issue , 2004, Pages

REDTOP-2: Rocket engine design tool featuring engine performance, weight, cost, and reliability

Author keywords

[No Author keywords available]

Indexed keywords

C++ PROGRAMMING LANGUAGE; COMBUSTION PRESSURE; COMPUTING ENGINES; COMPUTING PLATFORM; COST MODELS; DESIGN OPTION; ENGINE CONFIGURATION; ENGINE DEVELOPMENT; ENGINE PERFORMANCE; ENGINE WEIGHT; ENGINEERING DESIGN; ENGINEERING TOOLS; EXECUTION TIME; FLOW CONDITION; FLOW-RATE; FLOWPATH; LIQUID PROPULSION; MAIN COMPONENT; MODELING APPROACH; MODELING TOOL; OBJECT ORIENTED; OPTIMAL PERFORMANCE; PHYSICS-BASED ANALYSIS; POWER BALANCE; PRELIMINARY DESIGN; PRODUCTION COST; RELIABILITY METRICS; SEA-LEVEL; SPACE TRANSPORTATION SYSTEM; SPECIFIC IMPULSE; TOPDOWN;

EID: 77957835525     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (16)

References (8)
  • 1
    • 0007074523 scopus 로고
    • Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications
    • Oct
    • Gordon, S. and McBride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA Reference Publication 1311, Oct. 1994.
    • (1994) NASA Reference Publication , vol.1311
    • Gordon, S.1    McBride, B.J.2
  • 6
    • 69249126095 scopus 로고    scopus 로고
    • Spaceliner 100 Candidate Technology White Paper on Long-Life, High Thrust/Weight LOX/Hydrogen Engine
    • Levack, D., Spaceliner 100 Candidate Technology White Paper on Long-Life, High Thrust/Weight LOX/Hydrogen Engine, Boeing-Rocketdyne.
    • Boeing-Rocketdyne
    • Levack, D.1
  • 7
    • 0002228666 scopus 로고    scopus 로고
    • Lower Costs for Highly Reusable Space Vehicle
    • March
    • Mankins, J. C, "Lower Costs for Highly Reusable Space Vehicle," Aerospace America, March 1998, pp.36-42
    • (1998) Aerospace America , pp. 36-42
    • Mankins, J.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.