The combustion model of micro-void propellant is presented in this paper. The control equations for stable burning of propellant are set up.
建立了一个描述微孔推进剂燃烧的模型，并得到了推进剂稳定燃烧时的控制方程组。
The combustion model of micro-void propellant is presented in this paper. The control equations for stable burning of propellant are set up.
建立了一个描述微孔推进剂燃烧的模型，并得到了推进剂稳定燃烧时的控制方程组。
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