发明名称 DEPLOYMENT APPARATUS FOR LANDING A SPACE EXPLORATION SATELLITE
摘要 PURPOSE: A deployment device for landing a space exploring satellite is provided to improve utilization of an inner space of the space exploring satellite by reducing a space occupied inside the space exploring satellite through supplying hinge rotation structure. CONSTITUTION: A deployment device for landing a space exploring satellite comprises a first support rod(100), a second support rod(200), a hinge bracket(300), and an elasticity deployment unit(400). The second support rod is installed to be rotated by the structure of the space exploring satellite. The hinge bracket connects the first support rod and the second support rod and is equipped on the first support rod and the second support rod to be hinge-rotated. The elasticity deployment unit surrounds the first support rod and rotates the second support rod and the hinge bracket with respect to the first support rod by elastically pressurizing the hinge bracket when the restricting state of the second support rod is released.
申请公布号 KR20130060855(A) 申请公布日期 2013.06.10
申请号 KR20110127134 申请日期 2011.11.30
申请人 INDUSTRY-UNIVERSITY COOPERATION FOUNDATION KOREA AEROSPACE UNIVERSITY;KOREA AEROSPACE RESEARCH INSTITUTE 发明人 PARK, JUNG SUN;KIM, HYUN DUK;KIM, SUNG HOON;LIM, JAE HYUK
分类号 B64G1/22;B64C25/10;B64G1/14;B64G1/16 主分类号 B64G1/22
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