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公开(公告)号:KR100775988B1
公开(公告)日:2007-11-15
申请号:KR1020060105606
申请日:2006-10-30
Applicant: 한국항공우주연구원
CPC classification number: B64G1/66 , B64G2001/1028
Abstract: An optical loading device of an observation satellite is provided to effectively absorb thermal load generated in various directions. An optical loading device of an observation satellite includes a coupling unit(500). The coupling unit includes a first coupling part(510), a second coupling part(530), and a blade(550). The first coupling part is coupled to a platform. The second coupling part is coupled to a main body of the observation satellite. The blade connects the first coupling part and the second coupling part. Fastening grooves(510a) are formed in horizontal directions of the first coupling part. Fastening grooves(530a) are formed in vertical directions of the second coupling part. The coupling unit is connected to a main body of the platform.
Abstract translation: 提供了一种观测卫星的光学加载装置,以有效吸收在各个方向产生的热负荷。 观测卫星的光学加载装置包括耦合单元(500)。 联接单元包括第一联接部分(510),第二联接部分(530)和叶片(550)。 第一耦合部分耦合到平台。 第二耦合部分耦合到观测卫星的主体。 叶片连接第一联接部分和第二联接部分。 紧固槽(510a)在第一联接部的水平方向上形成。 紧固槽(530a)在第二联接部的垂直方向上形成。 联接单元连接到平台的主体。