Satellite launching method and satellite fixing device

Abstract

The embodiment of the invention provides a satellite launching method. The method comprises the steps: fixing a plurality of plate-shaped satellites in a stacked manner through a satellite fixing device, enabling the plurality of satellites to be carried on a rocket, removing the fixing of the satellite fixing device to the plurality of plate-shaped satellites, and enabling the plurality of plate-shaped satellites to be scattered. Moreover, the embodiment of the invention further provides a satellite fixing device. The satellite fixing device comprises a plate-shaped satellite mounting platform, a central supporting rod, a plurality of pressing limiting supporting rods, a plurality of transverse pull rods and a locking and releasing structure, the space of a rocket fairing can be fully utilized by the satellite fixing device structure, and satellite launching can meet the requirement of large-scale satellite launching deployment through a satellite launching method.

Description

technical field [0001] Embodiments of the present disclosure generally relate to the field of satellite launching, and more specifically, relate to a satellite launching method and a satellite fixing device. Background technique [0002] The use of satellites has a profound impact on the development of all aspects of society, such as economy, science, information, security, and humanities. Therefore, the satellite launch technology has been developed rapidly, from one rocket and one satellite to the launch method of one rocket and multiple satellites. The satellite launch method of one arrow and multiple satellites is an efficient way of launching spacecraft, which can make full use of the rocket’s Carrying capacity and reduced launch costs have good practical value for multi-satellite networking. [0003] In the satellite launch technology, the satellite fixing device is particularly important, which is docked and fixed with the rocket, and provides a mechanism for the sat...

AI Technical Summary

Problems solved by technology

The satellite fixing devices in the prior art are mainly developed and designed for a single satellite. The space utilization rate of the fairing of the rocket is low, and the requirements for large-scale satellite launch and deployment are not considered. Usually, the operation is difficult, and it is difficult to carry out rapid and large-scale deployment at the launch site. The docking of satellite rockets, and the design of the docking, installation and separation of satellite rockets is more complicated, and the working mechanism is different, making it difficult to ensure the reliability of all satellites' fixation and separation at the same time when launching a large number of satellites

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