公开(公告)号：KR101338178B1

公开(公告)日：2013-12-09

申请号：KR1020130092063

申请日：2013-08-02

Applicant: 국방과학연구소

Inventor： 이건하 ,  황철규 ,  정성학 ,  이재준 ,  양원혁

IPC: F42B10/20 ,  F42B10/64 ,  F42B15/00

CPC classification number: F41F3/052 ,  F41F1/00

Abstract: The present invention relates to restriction release apparatus of a portable guided missile. Disclosed is the restriction release apparatus including a cooling gas container assembly, which provides gas used for cooling an explorer; a branch block, which distributes the gas to the explorer; and a restriction release device of a portable guided missile, which releases the restriction of the portable guided missile by using the pressure of the gas provided from the branch block.

Abstract translation: 本发明涉及便携式导弹的限制解除装置。 公开了一种包括提供用于冷却探险者的气体的冷却气体容器组件的限制释放装置; 一个分支块，将气体分配给探险者; 以及便携式导弹的限制释放装置，其通过使用从分支块提供的气体的压力来释放便携式导弹的限制。

公开(公告)号：KR101330213B1

公开(公告)日：2013-11-18

申请号：KR1020130105472

申请日：2013-09-03

Applicant: 국방과학연구소

Inventor： 정성학 ,  황철규 ,  이영수 ,  김상식 ,  양원혁

IPC: F42B35/00 ,  F42B35/02 ,  F42B30/08

CPC classification number: F41G7/007 ,  F41G7/001 ,  F42B15/01

Abstract: The present invention provides a device for assembling and testing a portable guided missile which includes a platform with a rail extended in the first direction; a portable guide missile which fixes module which fixes the portable guide missile by covering and is driven to be rotated in the second direction parallel to the ground surface and in the third direction perpendicular to the ground surface; a launching tube fixing module which fixes a portable guide missile launching tube and is moved along the rail by being mounted on the platform; a front table which is arranged by being separated from the platform in the first direction; an image tracking unit which collects data by tracking a target on the front table which is acquired by a seeker mounted on the portable guide missile; and a driving unit which drives the portable guide missile fixing module based on the data. [Reference numerals] (AA) Operate a mock target;(BB) Spot the mock target in move and lock on the target;(CC) Track the target and check the eye line information;(DD) Track the target;(EE) Check the performance of a guided missile;(FF) Gimbal;(GG) Give an operation command;(HH) Check the gimbal to be controlled;(II) Target tracking information;(JJ) Additional data

Abstract translation: 本发明提供了一种用于组装和测试便携式导弹的装置，其包括具有沿第一方向延伸的轨道的平台; 便携式导弹，其固定通过覆盖固定便携式导弹的模块，并被驱动沿平行于地面的第二方向和垂直于地面的第三方向旋转; 发射管固定模块，其固定便携式导弹发射管，并通过安装在平台上沿着轨道移动; 前台，其沿第一方向与平台分离; 图像跟踪单元，其通过跟踪由安装在便携式导弹上的探测器获取的前台上的目标来收集数据; 以及基于该数据驱动便携式引导导弹固定模块的驱动单元。 （参考号）（AA）操作模拟目标;（BB）瞄准移动中的模拟目标并锁定目标;（CC）跟踪目标并检查眼线信息;（DD）跟踪目标;（EE） 检查导弹的性能;（FF）Gimbal;（GG）给出操作命令;（HH）检查待控制的万向节;（II）目标跟踪信息;（JJ）附加数据