Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

No-cable on-orbit service receivable satellite

A satellite and satellite attitude technology, applied in the field of cable-free and acceptable on-orbit service satellites, can solve the problems of constrained configuration layout, lack of pertinence in satellite design, flexibility and scalability, and increase the difficulty of on-orbit replacement. Achieve the effects of eliminating constraints, prolonging the life of satellites, and realizing replenishment

Inactive Publication Date: 2017-07-07
BEIJING INST OF SPACECRAFT SYST ENG
View PDF5 Cites 14 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In the existing technology, the constraints of the traditional satellite data network on the satellite system structure and configuration layout make the satellite design lack of pertinence, flexibility and scalability, and the weight of the interface hardware and cables connecting each subsystem in the satellite accounts for 10% to 15% of the overall weight of the satellite, which severely restricts the configuration layout and increases the difficulty of on-orbit replacement

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • No-cable on-orbit service receivable satellite
  • No-cable on-orbit service receivable satellite
  • No-cable on-orbit service receivable satellite

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0027] It should be understood that the satellite having the function of receiving on-orbit services of the present invention includes a satellite body, an on-orbit replaceable module, a passive docking mechanism, and a wireless information system. The satellite body is the main support structure, the replaceable module and passive docking mechanism are arranged outside the satellite, and the wireless information system realizes the management and data exchange of each component of the platform. On the basis of ensuring simple configuration, economic feasibility and compact size, it has the ability to accept on-orbit module replacement and on-orbit refilling. The invention adopts the design mode of wireless communication in the satellite, eliminates the constraints of the communication network wiring on the structure and configuration of the satellite system, and has the capability of module plug-and-play, thereby facilitating the implementation of on-orbit module replacement. ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a no-cable on-orbit service receivable satellite. The no-cable on-orbit service receivable satellite comprises a satellite body, a changeable module, a passive docking mechanism and a wireless communication system, wherein the satellite body is used as a main supporting structure, the changeable module is placed outside the satellite body to be convenient for module changing, the passive docking mechanism is used for receiving on-orbit gas and liquid filling, and the wireless communication system is used for realizing management and data exchanging of each part of a platform; and real-time access and removal of each module within the satellite are supported by using a wireless bus. Therefore, according to the no-cable on-orbit service receivable satellite, the changing of an on-orbit module can be convenient to operate, the service life of the satellite is actually prolonged, the adaptation of the satellite to multiple tasks is actually enhanced, restriction of communication network wiring to the structure, configuration and layout of a satellite system is eliminated, the configuration and layout of a satellite module can be designed according to application needs, the module is very convenient to detach and mount, a plug-and-play capacity is realized, the on-orbit module changing task is very easily realized and easily-consumed materials are supplemented so that the service life of the satellite is further prolonged.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and relates to a cableless acceptable on-orbit service satellite, which can realize management and data exchange of various components of the platform through a wireless information system, can accept on-orbit module replacement, and can also accept on-orbit add-ons. Note. Background technique [0002] Spacecraft on-orbit service refers to a type of space operation that involves extending the life of various spacecraft and improving the ability to perform tasks through the cooperation of humans, robots or both in space. On-orbit module replacement and on-orbit filling are the most typical efficiency-enhancing on-orbit service methods. Through module replacement and on-orbit refueling, the application efficiency of the spacecraft can be restored, maintained or improved, and the replacement and replenishment of faulty modules, consumables, etc. can be realized, so as to ensure the normal operat...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/64B64G1/66
CPCB64G1/10B64G1/646B64G1/66B64G1/223
Inventor 谭春林石军刘永健刘育强
Owner BEIJING INST OF SPACECRAFT SYST ENG
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products