SPACECRAFT CAPTURE MECHANISM
    2.
    发明申请
    SPACECRAFT CAPTURE MECHANISM 有权
    空间捕获机制

    公开(公告)号:US20150314893A1

    公开(公告)日:2015-11-05

    申请号:US14703709

    申请日:2015-05-04

    IPC分类号: B64G1/10 B64G1/22 B64G1/64

    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.

    摘要翻译: 本发明提供一种用于捕获和锁定到位于航天器/卫星的外表面上的马尔曼法兰的捕获机构。 捕获机制实现了通过将所涉及的两个基本动作分为两个独立机制来快速捕获客户航天器的目标。 一种机制可以快速掌握目标,而另一种机制刚性化,从而确保目标被保持牢固。