Control mechanism for aerodynamic rudders of solid propellant rocket engines

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  机译： 用于测试固体推进剂火箭发动机，固体推进剂火箭发动机和实施方法的测试方法

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  机译： 用于测试固体推进剂火箭发动机，固体推进剂火箭发动机和实施方法的测试方法

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  机译： 用于测试固体火箭发动机，固体火箭发动机的测试方法和实施该方法的系统

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