Liquid rocket engine performance assessment in the context of small launcher optimisation
作者: Alexandru-Iulian ONEL Oana-Iuliana POPESCU Ana-Maria NECULAESCU Tudorel-Petronel AFILIPOAE Teodor-Viorel CHELARU
作者单位: 1INCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, 061126, Bucharest, Romania,
2“POLITEHNICA” University of Bucharest, Faculty of Aerospace Engineering, Str. Gheorghe Polizu 1-7, 011061, Bucharest, Romania
刊名: INCAS BULLETIN, 2019, Vol.11 (3)
来源数据库: National Institute of Aerospace Research
DOI: 10.13111/2066-8201.2019.11.3.12
关键词: Rocket propulsionSpecific impulseNonlinear surface fittingSmall launchersMultidisciplinary optimisationMathematical model
原始语种摘要: The paper presents a fast mathematical model that can be used to quickly asses the propulsive characteristics of liquid propelled rocket engines. The main propulsive parameters are computed using combustion surfaces obtained after a nonlinear data fitting analysis. This approach is much more time efficient than using standard codes which rely on frequent calls of the Fuel Combustion Charts and interpolating their data. The tool developed based on the proposed mathematical model can be used separately or it can be integrated in a multidisciplinary optimisation algorithm for a preliminary microlauncher design.
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关键词翻译
关键词翻译
  • engine 发动机
  • interpolating 内插
  • rocket 火箭
  • mathematical 数学的
  • performance 性能
  • fitting 匹配
  • efficient 有用的
  • propulsive 推进的
  • frequent 时常的
  • propelled 推进的