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膨胀循环发动机起动过程研究
引用本文:肖立明,罗巧军. 膨胀循环发动机起动过程研究[J]. 火箭推进, 2007, 33(1): 7-11
作者姓名:肖立明  罗巧军
作者单位:北京航天动力研究所,北京,100076
摘    要:针对膨胀循环发动机起动过程的计算问题,基于模块化建模方法,研究了各组件的数学和仿真模型,运用Simulink工具箱,编制了针对液体火箭发动机系统起动过程计算所需的各个模块库。在此基础上,对膨胀循环发动机系统的起动过程进行了仿真研究,分析了起动过程的影响因素。

关 键 词:液体火箭发动机  膨胀循环  起动过程  Simulink  数值仿真
修稿时间:2006-09-112006-12-30

Investigation on start-up process of expander cycle liquid propellant rocket engine
Xiao Liming,Luo Qiaojun. Investigation on start-up process of expander cycle liquid propellant rocket engine[J]. Journal of Rocket Propulsion, 2007, 33(1): 7-11
Authors:Xiao Liming  Luo Qiaojun
Affiliation:Beijing Aerospace Propulsion Institute, Beijing 100076, China
Abstract:A research of modeling and simulation for the start-up process of expander cycle liquid propellant rocket engine (LPRE) is carried out in this paper. Based on the module modeling means, the expander cycle LPRE is disassembled into some typical components and their mathematical simulation models are researched. By utilizing the Simulink toolbox, various module libraries needed by the calculation of the transient process of LPRE system are programmed. The libraries lay a foundation for the continuative numerical simulation work. Then, the simulation investigation on the start-up process of the expander cycle LPRE is carried out and the influence factors in the start-up process are investigated.
Keywords:liquid propellant rocket engine  expander cycle  start-up process  Simulink  numerical simulation
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