Fairing-main satellite integrated large-caliber deployable spacecraft

A technology of fairings and spacecraft, applied in the field of spacecraft, can solve the problems of low economic benefits of fairings, large fuel consumption of fairings, and limited degrees of freedom, etc., to achieve high versatility, improve advanced nature, and increase degrees of freedom.

Active Publication Date: 2018-03-13
SHANGHAI SATELLITE ENG INST
View PDF5 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

From the perspective of aerospace economy, the economic benefits of the fairing are relatively low
The fairing not only consumes a lot of fuel during the launch process, but more importantly, the fairing greatly restricts the freedom of various spacecraft structural designs, and becomes an insurmountable barrier for large-scale and new spacecraft structural designs

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
  • Fairing-main satellite integrated large-caliber deployable spacecraft
  • Fairing-main satellite integrated large-caliber deployable spacecraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] The preferred embodiments of the present invention are given below in conjunction with the accompanying drawings to describe the technical solution of the present invention in detail.

[0014] like Figure 1 to Figure 2 As shown, the large-diameter expandable spacecraft with integrated fairing main star of the present invention includes a spacecraft main star 50, a fairing 40, a fairing top cover 20, a flexible cable net 30, and a deployment mechanism 21. The spacecraft main star 50 is connected with the deployment mechanism 21. The fairing 40 is connected, the fairing 40 is connected with the flexible cable net 30, the plurality of fairing top covers 20 are connected with the deployment mechanism 21, the plurality of fairing top covers 20 are hinged with the fairing 40, and the flexible cable net is used to connect the fairing The fairing forms a large-diameter antenna together with the fairing; the fairing folds up to rectify during the launch process; the top cover o...

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 fairing-main satellite integrated large-caliber deployable spacecraft. The fairing-main satellite integrated large-caliber deployable spacecraft comprises a spacecraft main satellite and the like, wherein the spacecraft main satellite is connected with a fairing through a deploying mechanism; the fairing is connected with a flexible cable net; a plurality of fairing top covers are connected with the deploying mechanism, and are connected with the fairing through hinges; the flexible cable net is used for being connected with the fairing, and a large-caliber antenna isformed by the flexible cable net and the fairing; in a launching process, the fairing is furled to achieve the effect of rectification; in the launching process of the spacecraft, the fairing top covers achieve the effect of rectification; after being in an orbit, the fairing is deployed under the driving of the deploying mechanism; and the deploying mechanism is used for being connected with thefairing and the spacecraft main satellite and driving the fairing to be deployed. According to the fairing-main satellite integrated large-caliber deployable spacecraft disclosed by the invention, a large-caliber satellite-mounted antenna design is realized, the limit to the large-caliber satellite-mounted antenna is removed, and the formset surface error of the large-caliber satellite-mounted antenna is effectively controlled.

Description

technical field [0001] The invention relates to a spacecraft, in particular to a large-diameter deployable spacecraft with a fairing main star integrated. Background technique [0002] The satellite antenna refers to the antenna loaded on the artificial satellite. It is the input and output device of the satellite signal. The satellite communication is realized through the mutual transmission of electromagnetic waves between the satellite antenna and the earth station antenna. With the rapid development of my country's space technology, such as communication satellite technology, relay satellite and earth observation technology, the demand for spaceborne antennas is increasing day by day, and the requirements for its caliber and precision technical indicators are also getting higher and higher. However, at this stage, the functions and overall layout of any satellite are limited by the envelope space of the launch vehicle. The limited space of the fairing forces the develop...

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): B64G1/22
CPCB64G1/22B64G1/222
Inventor 李昊孔祥森周静张娇赵川
Owner SHANGHAI SATELLITE ENG INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap