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首页> 外文期刊>Propellants, Explosives, Pyrotechnics >The Starting Transient in a Gas-Generator Hydrid Rocket Motor
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The Starting Transient in a Gas-Generator Hydrid Rocket Motor

机译:气体发生器混合动力火箭发动机的起动瞬态

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摘要

A model for hte prediction of the starting transient in a gas-generator hydrid motor is presented. The model considers essential desin parameters such as complex grain configuration, boundary conditions, erosive burning rate, as well as spatially and temporally variable thermodynamic properties of both condensed material and gas flow. The developed numerical code fo rthe model solution demonstrates a strong capabiltiy for solving time-dependent fluid dynamics problems and can be particularly useful for internal ballistics considerations as well as for stability analysis. Several scenarios for starting transients of a large-size motor are considered and worst case events are identified.
机译:提出了一种用于预测发电机发电机液压马达起动瞬态的模型。该模型考虑了必要的设计参数,例如复杂的晶粒构型,边界条件,侵蚀燃烧速率以及冷凝材料和气流的时空热力学特性。模型解决方案的已开发数字代码显示出解决时变流体动力学问题的强大能力,对于内部弹道考虑因素和稳定性分析特别有用。考虑了启动大型电机瞬态的几种情况,并确定了最坏情况的事件。

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