Separable micro and nano-satellite configuration

Abstract

The invention discloses separable micro and nano-satellite configuration which comprises a satellite body, a plurality of separate release sub-satellites, mechanical net claws, a flexible solar cell array and a variable-structure mechanical arm. The separable micro and nano-satellite configuration has the advantages that the integral separable micro and nano-satellite configuration is in such a configuration form that a primary satellite carries the multiple sub-satellites, and functions of separately releasing and hovering the micro and nano-satellites can be realized; the efficiency of the solar cell array can be improved owing to combined configuration comprising flexible solar wings and the variable-structure mechanical arm; mechanical net claw mechanisms are carried on the micro and nano-satellites, so that a function of capturing space targets can be realized; the separable micro and nano-satellite configuration is provided with a plurality of stereoscopic vision imaging cameras, so that a stereoscopic monitoring function can be realized; attitude maneuver and attitude stabilization of the micro and nano-satellites can be implemented by the aid of a solid miniature propulsion technology, so that the sub-satellite separate release control ability can be improved; the separable micro and nano-satellite configuration is applicable to fifty-kilogram-level micro-miniature artificial earth satellites on near-earth orbits and is also applicable to micro-satellite networking, scientific detection aircrafts and relevant micro and nano-satellite space demonstration and experiments.

Description

technical field [0001] The invention belongs to the field of aerospace vehicle structure design, and in particular relates to a detachable micro-nano-satellite configuration. Background technique [0002] The space demonstration test refers to the integration of advanced new technology test loads and newly developed stand-alone products through the satellite platform, so that it can verify the function and performance of payloads and stand-alone products in the space environment. With the development of productization, serialization, and miniaturization of my country's micro-nano satellites, more and more new payloads and stand-alone products need to obtain technological breakthroughs through space demonstration tests, requiring satellite configurations to adapt to modularization and detachable release , Short development cycle and low cost requirements. The payload and stand-alone equipment of the traditional satellite configuration are permanently fixed on the satellite an...

AI Technical Summary

Problems solved by technology

The payload and stand-alone equipment of the traditional satellite configuration are permanently fixed on the satellite and

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