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公开(公告)号:EP3137379A4
公开(公告)日:2017-12-27
申请号:EP15785813
申请日:2015-05-04
CPC分类号: B64G4/00 , B64G1/1078 , B64G1/222 , B64G1/646 , B64G2004/005
摘要: The present invention provides a capture mechanism for capturing and locking onto the Marman flange located on the exterior surfaces of spacecraft/satellites. The capture mechanism achieves its goal of quickly capturing a client spacecraft by splitting the two basic actions involved into two separate mechanisms. One mechanism performs the quick grasp of the target while the other mechanism rigidises that grasp to ensure that the target is held as firmly as desired.