small solid rocket impulse engine 小型固体火箭脉冲发动机
impulse rocket engine 脉冲式火箭发动机
impulse type engine 脉动喷气发动机
impulse duct engine 脉冲式喷气发动机
impulse-rocket engine 脉冲式火箭发动机
micro impulse jet engine 微型脉冲发动机
engine specific impulse 发动机比冲
Aiming at the impulse engine in the trajectory correction projectile, one dynamic experiment method is put forward to measure the correction ability of the impulse engine.
针对弹道修正技术中应用的脉冲发动机,设计了一种用于验证发动机修正能力的动态实验方法。
It is pointed out that the expectant trajectory control effect can be achieved by the priority selection of the structural parameter and operative parameter of impulse engine.
分析表明,通过优选脉冲发动机的结构参数和工作参数可以达到预期的弹道控制效果。
So the research is important to the selection of the fire time and number of the impulse engine and serves as theory reference.
研究结果对脉冲发动机的点火起控点选择以及脉冲发动机的个数选择都有一定参考价值。
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