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Rocket catapult with direct mechanically actuated ignition of rocket motor
Rocket catapult with direct mechanically actuated ignition of rocket motor
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机译:火箭弹射器,直接机械驱动火箭发动机点火
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摘要
An improved rocket catapult is disclosed for use in aircraft ejection systems permitting direct ignition of the rocket motor by a mechanically- actuated igniter situated in proximity to the rocket motor grain and which is actuated when the rocket motor has traveled a predetermined distance during the catapult phase of its operation.
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