推进技术 ›› 1992, Vol. 13 ›› Issue (4): 22-27.

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变推力液体火箭发机系统仿真软件的研究

吕志信   

  1. 国防科技大学
  • 发布日期:2021-08-15

A RESEARCH ON THE SIMULATION SOFTWARE OF A VARIABLE THRUST LIQUID PROPELLANT ROCKET ENGINE SYSTEM

  1. National University of Defense Technology
  • Published:2021-08-15

摘要: 闸明了变推力液体火箭发动机系统仿真软件设计的指导思想,介绍了软件的结构,着重叙述了典型部件的运算模块。最后,简单地介绍丁在实现该软件时的一些技术处理。

关键词: 可变推力;液体推进剂火箭发动机;系统模型;仿真技术

Abstract: This paper is a summary of the research work on the simulation of a variable thrusl rocket engine system. The design ideals of software arc explained. The software structure is introduced and the calculation module of typical components is illustrated in detail. At last, some technical problems on software realization are simply handled.

Key words: Variale thrust;Liquid rocket engine;System model;Simulation technique