该文提出描述液体工质电热化学发射装置中燃烧过程的理论模型。
A theoretical model has been presented to describe the combustion process in a liquid propellant electrothermal chemical launcher.
消融毛细管等离子体发生器是电热化学发射系统中重要的组成部分。
Ablation capillaries plasma generator is a basic composition element in an electrothermal launching system.
在电热化学发射中，等离子体发生器的放电过程是电能转化为热能的重要阶段。
Discharge of plasma generator in electrothermal launchers is a main process of converting electrical energy to heat energy.
利用该模型对电热化学发射内弹道过程进行了数值模拟，并将模拟结果与实验数据进行了分析比较，结果表明模拟结果与实验数据基本吻合。
The launching process in interior ballistics is numerically simulated, the comparison of simulation results with experimental ones indicates that the simulation agreed well with the experiments.
利用该模型对电热化学发射内弹道过程进行了数值模拟，并将模拟结果与实验数据进行了分析比较，结果表明模拟结果与实验数据基本吻合。
The launching process in interior ballistics is numerically simulated, the comparison of simulation results with experimental ones indicates that the simulation agreed well with the experiments.
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