推进技术 ›› 2004, Vol. 25 ›› Issue (2): 148-151.

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空间推进系统静动态特性仿真软件研究

李家文,张黎辉,张雪梅,金广明,魏彦祥   

  1. 北京航空航天大学宇航学院;北京100083;北京航空航天大学宇航学院;北京100083;北京航空航天大学宇航学院;北京100083;上海航天动力机械研究所 ;上海200233;上海航天动力机械研究所 ;上海200233
  • 发布日期:2021-08-15

Simulation software for the static and dynamic characteristics of space propulsion system

  1. School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Shanghai Inst. of Space Propulsion, Shanghai 200233, China;Shanghai Inst. of Space Propulsion, Shanghai 200233, China
  • Published:2021-08-15

摘要: 基于特征线法进行了双组元挤压式空间推进系统动态过程仿真方法的研究,提出了在动态过程仿真模型基础上建立和求解静态特性仿真模型的方法。编制了静动态特性仿真软件,通过对某空间推进系统进行的调整工况、模拟故障时的静动态特性仿真,验证了所提出的静动态特性仿真方法的可行性和实用性,该方法可以减少仿真所需的工作量。通过扩充元件库,能够对其它类型推进系统进行仿真。

关键词: 液体推进剂火箭发动机;推进系统;静态特性;动态特性;仿真

Abstract: Based on the method of characteristics, a simulation method for dynamic process of bipropellant pressure-fed space propulsion system was studied. A method of building and evaluating static characteristics simulation model was presented and it was based on the dynamic process simulation model. By simulating the static and dynamic characteristic of one space propulsion system, the feasibility and practicability of this method was validated. It may reduce the workload by this method. By appending components in the software, other propulsion systems can be simulated.

Key words: Liquid propellant rocket engine;Propulsion system;Static characteristics;Dynamic process;Simulation