发明名称 SATELLITE SEPARATION DEVICE
摘要 PURPOSE: A separating device for a satellite is provided to shorten a separating time in times of actuating using an elastic member and perform separation without damages to a satellite and a separating unit by minimizing impact. CONSTITUTION: A separating device for a satellite comprises first and second actuating units. A separating pin(10) fixes the satellite and a separating device. The first actuating unit separates the separating pin by linear movement and rotational movement by electricity. The guide(30) of the first actuating unit comprises a fixing hole(31). The fixing hole faces the fixing groove(11) of the separating pin. The constraint of a first steel ball(20) is released by the guide.
申请公布号 KR20110129231(A) 申请公布日期 2011.12.01
申请号 KR20100048755 申请日期 2010.05.25
申请人 INDUSTRY-UNIVERSITY COOPERATION FOUNDATION KOREA AEROSPACE UNIVERSITY 发明人 KIM, BYUNG KYU;LEE, MIN SU;PARK, HYUN JUN;JO, JAE UK;TAK, WON JUN
分类号 B64G1/64;B64G1/10;B64G1/22 主分类号 B64G1/64
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