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