Space rendezvous docking assembly

A docking device and space rendezvous technology, applied to the docking device of aerospace vehicles, etc., can solve problems such as danger, bulkiness, and difficulties for astronauts, and achieve the effects of reliable locking, effective docking, and simple docking and launching

Active Publication Date: 2014-10-01
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] It turns out that these tasks are mainly completed by astronauts, but these extravehicular activities will be subject to many restrictions: first, the strength and scope of work of astronauts are limited, and they cannot do anything about the installation of large-scale aerospace equipment (such as space stations); second, due to oxygen supply and There are dangerous reasons such as radiation in outer space, and the continuous working time of astronauts outside the cabin is limited; in addition, due to the existence of microgravity, high vacuum, strong radiation and tiny planetary bodies in space, it is difficult for astronauts to perform various operations in the space environment. It is very difficult and dangerous; at the same time, in order to support the extravehicular activities of astronauts, a huge and complex environmental control system and life support system are required, which will inevitably bring huge expenses.

Method used

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Embodiment Construction

[0024] The following combination Figure 1 to Figure 8 , a preferred embodiment of the present invention is described in detail.

[0025] The space rendezvous and docking device provided by the present invention includes an anode assembly and a cathode assembly, the anode assembly is installed on a serviced spacecraft such as a satellite or other space mobile aircraft, and the cathode assembly is installed on a service vehicle such as a space platform on the spacecraft. Such as figure 2 As shown, the space rendezvous and docking device 13 in this embodiment is installed between the satellite 14 and the space platform 15, wherein the anode assembly is installed at the center of the satellite 14, and is connected with the satellite 14 and connected with the satellite front plate Vertically, the cathode assembly is installed in the parking position on the space platform 15 and connected with the space platform 15; by inserting the anode assembly into the inside of the cathode ...

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Abstract

The invention relates to a space rendezvous docking assembly which comprises an anode assembly and a cathode assembly. The anode assembly is installed on a served spacecraft, the cathode assembly is installed on a serving spacecraft, the anode assembly is inserted into the cathode assembly and is locked by the cathode assembly, the safe and reliable rendezvous docking between the served spacecraft and the serving spacecraft is achieved, and thus different in-obit service tasks are completed.

Description

technical field [0001] The invention relates to a space rendezvous and docking device, in particular to a docking and docking device used between a satellite and a platform, and belongs to the technical field of space rendezvous and docking. Background technique [0002] With the advancement of space technology, the number of satellites and spacecraft launched every year around the world is increasing, and the diversity and complexity of space work are also increasing rapidly, so the demand for extravehicular activities is also increasing. For example, the capture, maintenance, fuel replenishment and module replacement of in-orbit spacecraft, as well as scientific experiments on the outer space environment, and extravehicular activities such as cleaning up space junk. [0003] It turns out that these tasks are mainly completed by astronauts, but these extravehicular activities will be subject to many restrictions: first, the strength and scope of work of astronauts are limit...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
Inventor 胡坤韩飞卢山
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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