The invention relates to an exposed load supporting system for a spacecraft. The exposed load supporting system comprises a hollow shell (1), a guide structure (2) arranged on a first side face (11) of the shell (1), an interface supporting device (3) arranged on the shell (1) and an auxiliary locking device (4) used for clamping test load equipment. The auxiliary locking device (4) and the guidestructure (2) are arranged on the same side of the shell (1); and a plurality of connecting through holes (5) penetrating through the two opposite sides of the shell are formed in the first side surface (11). The exposed load supporting system has the locking/unlocking function, on-orbit replacement of test load equipment can be achieved under the cooperation of astronauts and mechanical arms, thespace outside a cabin of a spacecraft can be repeatedly utilized, and space resources of the spacecraft are effectively saved.
本发明涉及一种用于航天器的暴露载荷支持系统,包括:中空的壳体(1),设置在所述壳体(1)的第一侧面(11)上的导向结构(2),以及设置在所述壳体(1)上的接口支持装置(3),用于夹紧试验载荷设备的辅助锁紧装置(4);所述辅助锁紧装置(4)与所述导向结构(2)设置与所述壳体(1)的同一侧;所述第一侧面(11)上设置有贯穿所述壳体相对两侧的多个连接通孔(5)。本发明的暴露载荷支持系统具有锁紧/解锁功能,在航天员和机械臂的配合下可以实现试验载荷设备的在轨更换,能够重复利用航天器的舱外空间,有效地节约了航天器的空间资源。
Exposed load support system for spacecraft
一种用于航天器的暴露载荷支持系统
2020-05-19
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
Connecting device applied between outboard handle of spacecraft and exposed load
European Patent Office | 2015
|Spacecraft Sustained Load Fracture Control
NTIS | 1991
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