A STUDY ON SYSTEM RESPONSE FOR LIQUID PROPELLANT STAGED COMBUSTION CYCLE ROCKET ENGINE

Zhang Lihui; Zhang Zhenpeng

Chinese

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A STUDY ON SYSTEM RESPONSE FOR LIQUID PROPELLANT STAGED COMBUSTION CYCLE ROCKET ENGINE

更新时间：2026-07-07

- A STUDY ON SYSTEM RESPONSE FOR LIQUID PROPELLANT STAGED COMBUSTION CYCLE ROCKET ENGINE
- Vol. 14, Issue 4, (1999)
- 作者机构：
  
  北京航空航天大学
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：1999
- 稿件说明：
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Zhang Lihui, Zhang Zhenpeng. A STUDY ON SYSTEM RESPONSE FOR LIQUID PROPELLANT STAGED COMBUSTION CYCLE ROCKET ENGINE[J]. 1999, 14(4).
DOI：

Zhang Lihui, Zhang Zhenpeng. A STUDY ON SYSTEM RESPONSE FOR LIQUID PROPELLANT STAGED COMBUSTION CYCLE ROCKET ENGINE[J]. 1999, 14(4). DOI：

摘要

Abstract

A feeding system of a pump-fed Liquid Propellant Staged Combustion Cycle Rocket Engine (LPSCCRE) is taken as a research object.Its system physical model is constructed

and its nonlinear mathematical model is established.The nonlinear dynamic response of LPSCCRE is simulated with adaptive Runge-Kutta algorithm on the conditions of parameter variation and working regime regulation in wide range.Comparison of the obtained results with the test data shows that:The mathematical model is quite valid and calculation method meets the simulation requirements.

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