fast ignition phase 快速点火阶段
gas-phase ignition 气态点火
phase ignition 气态点火
ignition burning phase 点火燃烧段
solid phase ignition 固相点火
A thermal conduct model of ignition phase was established, with which the effect of various parameters on the ignition delay is analyzed.
建立了推进器点火过程热传导模型，利用该模型分析了不同因素对点火延迟时问的影响。
It proposes a way to obtain atmospheric radio frequency glow discharge with high stability and reduced power consumption by operating discharge in ignition phase.
通过短时间脉冲调制获得了将射频放电控制工作在放电起辉阶段，提出了一种新型的高稳定低功耗的常压放电技术。
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.
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。
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