发明名称 ADVANCED SPACECRAFT INTEGRATION DOLLY
摘要 PURPOSE: A dolly for satellite assembly is provided to ensure easy access to the whole part of a satellite and facilitate the manufacture and repair. CONSTITUTION: A lower platform(100) comprises a lower plate(110) and a plurality of support structures(120,130,140,150). The support structures are extended from the lower plate and comprise supporting units(122,132,142,152) and mobile tools(121,131,141,151). An upper platform(200) is arranged on the lower platform and comprises an access hole(230) which accepts at least a part of a satellite to permit access by an operator. The supporting units are moved up and down with a handle. The upper and lower platforms are selectively attached or detached.
申请公布号 KR20100018844(A) 申请公布日期 2010.02.18
申请号 KR20080077541 申请日期 2008.08.07
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 WOO, SUNG HYUN;IM, HYUK SOON;KIM, JIN HEE;MOON, HONG YOUL;CHUN, YONG SIK;LEE, SANG RYOOL
分类号 B64G1/10 主分类号 B64G1/10
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