在研制变推力火箭发动机的过程中，低工况时遇到了燃烧振荡问题，我们采用横向挡流板很好地解决了这个问题。

On the development process of the variable thrust rocket engine combustion vibra ions are encountered in the low working conditions, we solved this problem finely by lateral baffle.

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火箭泵的设计，优化的低和高推力。

Rocket pump designs optimized for low and high thrust.

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火箭泵的设计，优化的低和高推力。

Rocket pump designs optimized for low and high thrust.

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