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    • 4. 发明申请
    • Salvaging and Braking Device for Objects Flying Freely in Space
    • 在空间自由飞行的物品的救生和制动装置
    • US20130175401A1
    • 2013-07-11
    • US13824329
    • 2012-02-29
    • Juergen StarkeBernhard BischofJosef SommerMichael DumkeUwe Bruege
    • Juergen StarkeBernhard BischofJosef SommerMichael DumkeUwe Bruege
    • B64G1/40
    • B64G1/1078B64G1/007B64G1/40B64G1/62B64G1/646
    • In a recovery and braking device for objects flying freely in space, particularly for capturing satellites and other orbital objects, (at least one,) preferably a larger number of capturing units (2) are arranged on a spacecraft serving as a steerable carrier vehicle (1), wherein the capturing units are separable from the spacecraft, are equipped with a propellant charge of their own, and comprise a closeable capture net (4) releasably connected via a line (5). The carrier vehicle is equipped with position or attitude controlling engines (6), in order to achieve an orienting of the coupled mass configuration in preparation for the separation. In that regard, several capturing units can be combined into a series or parallel connection. After the oriented deployment/separation, the passive stability of the arrangement is utilized, taking into consideration the system behavior of the flexibly coupled objects, whereby sufficient position or attitude stability and accuracy is ensured even without active position or attitude control.
    • 在用于在空间中自由飞行的物体的恢复和制动装置中,特别是用于捕获卫星和其他轨道物体的(至少一个)优选地,较大数量的捕获单元(2)布置在用作可转向运载工具的航天器上 1),其中所述捕获单元可与所述航天器分离,配备有它们自己的推进剂装料,并且包括经由管线(5)可释放地连接的可关闭捕获网(4)。 载体车辆配备有位置或姿态控制发动机(6),以便实现耦合质量构造的取向以准备分离。 在这方面,几个捕获单元可以组合成串联或并联连接。 在定向部署/分离之后,考虑到灵活耦合的物体的系统特性,利用该装置的被动稳定性,由此即使没有主动位置或姿态控制也能确保足够的位置或姿态稳定性和准确性。