发明名称 DEVICE AND METHOD FOR TESTING SEPARATION TWO CANTILEVER TYPE BODIES
摘要 A device for testing separation of two cantilever type bodies is provided to realize environment similar to real flight environment generated when a launching tube is separated from a guided missile by freely controlling launching elevation within a predetermined angle by a rotation device. A device for testing separation of two cantilever type bodies comprises an imitation missile structure(100), a launching tube(110), a rotation device(120), a plurality of abrasion force imitation devices(180), a charging jig(170) and a pair of transportation rails(150,160). The imitation missile structure has a built-in projection engine. The launching tube is inserted into the imitation missile structure. The rotation device fixes a rear end of the imitation missile structure so as to control launching elevation within a predetermined angle. The plurality of abrasion force imitation devices is installed in an upper part of the imitation missile structure so as to control abrasion force between the imitation missile structure and the launching tube. The charging jig supports the launching tube so as to charge launching tube into the imitation missile structure. The pair of transportation rails support the charging jig to be moved in axial direction.
申请公布号 KR100750947(B1) 申请公布日期 2007.08.14
申请号 KR20060022976 申请日期 2006.03.13
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 KIM, HEUNG YOUL;JUN, YONG BUM;AHN, SUNG WOO
分类号 G01M99/00;G01M15/14 主分类号 G01M99/00
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