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Zero-damage low-consumption on-orbit continuous pushing and launching system

A sub-system and slide rail technology, applied in launch systems, aerospace equipment, space navigation equipment, etc., can solve the problems of high cost, high fuel consumption, harmful emissions, etc., achieve low cost, reduce launch cost, and facilitate storage Effect

Active Publication Date: 2021-08-13
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The above-mentioned "one-to-one", "multiple satellites with one arrow" and on-orbit launch modes have problems such as high fuel consumption, high cost and harmful emissions to varying degrees

Method used

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  • Zero-damage low-consumption on-orbit continuous pushing and launching system

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Embodiment Construction

[0039] In order to make the objects, technical solutions and advantages of the present invention, the spirit of the present invention will be described below with reference to the drawings and detailed description, and those skilled in the art will appreciate the embodiments of the present invention. When the techniques described by the present invention, variations and modifications can be made from the spirit and scope of the invention. An illustrative embodiment of the invention and a description thereof are for explaining the invention, but is not limited to the present invention.

[0040] Refer figure 1 In this embodiment, the present embodiment provides a push for storing a plurality of cubic stars and provides power for each cube star in the rail emission, by heating the solid-state phase change in the spectrometer, excited solid worker Instantaneous expansion, transforming into high-pressure gaseous works, high-pressure gaseous working fluid expansion work, cubic, so that ...

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Abstract

The invention provides a zero-damage low-consumption in-orbit continuous pushing and launching system. The system is composed of a satellite platform, a pushing and launching device and a plurality of cubesats. The satellite platform carries the pushing and launching device and dozens of hundreds of cubesats to be launched into an orbit from the ground and then operates in orbit, and the pushing and launching device continuously pushes the cubesats into transfer orbits flying to different target spacecrafts through carbon dioxide phase change expansion acting, so that multiple on-orbit service tasks such as on-orbit maintenance, on-orbit assembly and space debris removal are completed. The system is a novel green, environment-friendly, safe and efficient on-orbit launching mode, fuel consumption and harmful substance emission are greatly reduced, and energy conservation and emission reduction in spaceflight activities are greatly promoted. The on-orbit launching mode of on-orbit continuous push launching changes the task mode of the existing space on-orbit service, and has great significance for national space facility maintenance and space safety guarantee.

Description

Technical field [0001] The present invention relates to the general design of the spacecraft, and more particularly to a zero-damaged low consumption in the rail continuous urging system. Background technique [0002] With the continuous development of space technology and aerospace industry, in terms of rail add, rail maintenance, fragmentation and other spaces are growing in terms of rail service tasks, bringing new challenges to aerospace launch. [0003] The "one-to-one" mode fuel consumption of single space task is large, high cost, and it is difficult to complete a number of tasks in a short period of time. [0004] "One Arrow Multi-Star" mode and in the rail emission mode (referring to the release of the task satellite in the space station, freight spaceship, satellite, etc.), saves the carrying fuel consumption and cost to a certain extent. However, the task satellite needs to rely on the propulsion system (consumable propellant, etc.) to perform orbital transfer to compl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/00
CPCB64G1/005B64G1/6459B64G1/002B64G1/643B64G1/1081B64G1/10B64G1/641B64G1/645B64G1/223
Inventor 杨跃能胡文俊张朝衍张士峰段富强叶童黄淑锐韩毅尹聚祺
Owner NAT UNIV OF DEFENSE TECH