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MISSILE ACCELERATOR, AND MISSILE ACCELERATING METHOD

机译:导弹加速器和导弹加速方法

摘要

PROBLEM TO BE SOLVED: To provide an accelerator and an accelerating method capable of easily and consistently accelerating a missile at a high speed.;SOLUTION: The missile accelerator comprises a high energy driving gas generation unit 20 to generate high energy driving gas by compressing predetermined driving gas, a missile accelerating unit 30 having a missile to be accelerated by utilizing the expansion velocity of the high energy driving gas, and a high-pressure coupling 40 to connect the high energy driving gas generation unit 20 to the missile accelerating unit 30. A driving gas compression hole 21 of the high energy driving gas generation unit 20 is connected to a missile acceleration hole 31 in which the missile of the missile accelerating unit 30 is arranged via a connection hole 41 of the high-pressure coupling 40. The diameter of the connection hole 41 of the high-pressure coupling 40 is reduced from the high energy driving gas generation unit 20 to the missile accelerating unit 30.;COPYRIGHT: (C)2005,JPO&NCIPI
机译:解决的问题:提供一种能够容易且始终如一地高速使导弹加速的加速器和加速方法。解决方案:导弹加速器包括高能驱动气体产生单元20,其通过压缩预定量来产生高能驱动气体。驱动气体;导弹加速单元30,其具有通过利用高能驱动气体的膨胀速度而被加速的导弹;以及高压联接器40,其将高能驱动气体产生单元20连接至导弹加速单元30。高能驱动气体产生单元20的驱动气体压缩孔21经由高压联接器40的连接孔41连接至导弹加速孔31,导弹加速单元30的导弹布置在该导弹加速孔中。直径高压联接器40的连接孔41的高度从高能驱动气体产生单元20减小到导弹加速第30单元;版权:(C)2005,JPO&NCIPI

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