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[an error occurred while processing this directive]The Research of Start Dynamics for Rocket Engine
Received date: 2009-11-25
Online published: 2025-05-28
陈艳霞 , 关世玺 , 唐家鹏 . 火箭发动机起动过程动力学研究[J]. 弹箭与制导学报, 2010 , 30(5) : 131 -132,136 . DOI: 10.15892/j.cnki.djzdxb.2010.05.038
According to the new-developed liquid rocket engine feature,the dynamic mathematic model of main system component was built.Considering low temperature characteristics of the propellant,the start process of the engine was researched.The method of characteristics and classical Runge-Kutta was adopted for system model.Result shows that the model is reasonable,and provides criterion for judging whether the system can work steadily,and can be a guide for design,improvement and experiment.
Key words: liquid propellant rocket engine; start; dynamics; simulatio
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