公开(公告)号：US08028625B2

公开(公告)日：2011-10-04

申请号：US12366859

申请日：2009-02-06

申请人： Jai-Ha Kim ,  Dong-Ju Lee ,  Yang-Wook Hur ,  Ki-Soo Bae

发明人： Jai-Ha Kim ,  Dong-Ju Lee ,  Yang-Wook Hur ,  Ki-Soo Bae

IPC分类号： F42B15/36

CPC分类号： F42B15/36

摘要： Disclosed is a device for separating a propulsion system from a missile, the device including a locking unit configured to fix a propulsion system to a missile, a string disposed to cross a rear portion of the propulsion system to be broken by heat of the propulsion system, and an unlocking unit configured to unlock the missile by the broken string, whereby the number of additional components of an unlocking system can be reduced as many as possible so as to simplify the configuration of the apparatus, resulting in guaranteeing an enhanced performance of the missile, an easy assembly of the missile, and a reduction of a fabricating cost.

摘要翻译： 公开了一种用于将推进系统与导弹分离的装置，该装置包括构造成将推进系统固定到导弹的锁定单元，设置成跨越推进系统的后部以被推进系统的热量破坏的弦 以及解锁单元，其被配置为通过断线对所述导弹解锁，由此可以尽可能多地减少解锁系统的附加组件的数量，以便简化设备的配置，从而保证提高 导弹，易于组装的导弹，并减少制造成本。

公开(公告)号：US20100050897A1

公开(公告)日：2010-03-04

申请号：US12366859

申请日：2009-02-06

申请人： Jai-Ha KIM ,  Dong-Ju LEE ,  Yang-Wook HUR ,  Ki-Soo BAE

发明人： Jai-Ha KIM ,  Dong-Ju LEE ,  Yang-Wook HUR ,  Ki-Soo BAE

IPC分类号： F42B15/36

CPC分类号： F42B15/36

摘要： Disclosed is a device for separating a propulsion system from a missile, the device including a locking unit configured to fix a propulsion system to a missile, a string disposed to cross a rear portion of the propulsion system to be broken by heat of the propulsion system, and an unlocking unit configured to unlock the missile by the broken string, whereby the number of additional components of an unlocking system can be reduced as many as possible so as to simplify the configuration of the apparatus, resulting in guaranteeing an enhanced performance of the missile, an easy assembly of the missile, and a reduction of a fabricating cost.

摘要翻译： 公开了一种用于将推进系统与导弹分离的装置，该装置包括构造成将推进系统固定到导弹的锁定单元，设置成跨越推进系统的后部以被推进系统的热量破坏的弦 以及解锁单元，其被配置为通过断线对所述导弹解锁，由此可以尽可能多地减少解锁系统的附加组件的数量，以便简化设备的配置，从而保证提高 导弹，易于组装的导弹，并减少制造成本。