采用理论和实验相结合的方法确定冲击点火延迟时间可明显减少实验量。
The method combined the theory with the experiment may obviously decrease tests to determine shock ignition time.
建立了微型脉冲推力器点火启动模型，模型中考虑了两相流动和颗粒对推进剂表面的冲击传热。
Ignition start-up model of impulse micro-thruster is established, considering two phase flow and impact heat transfer of particle on the surface of propellant.
另外还对点火增长模型中的不同参数进行调整，定性地测定参数对冲击波起爆性能的影响。
In addition, the different parameters in Ignition and Growth model are adjusted in order to qualitatively examine the influence on shock initiation behavior made by the parameters.
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