Architecture for supporting ultrahigh power consumption of small satellite

A satellite, ultra-high technology, applied in the field of architecture that supports ultra-high power consumption, can solve the problems of large launch space, unfavorable for multiple people to work at the same time, and hindering the launch of small satellites.

Active Publication Date: 2020-12-08
HARBIN INST OF TECH
View PDF12 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

however, the larger cube volume requires a correspondingly larger launch space in the launch vehicle, thus preventing the launch of small satellites in a "multiple satellites with one rocket" approach
The cube-shaped structure is also not conducive to the simultaneous operation of multiple people in the process of small satellite assembly, which makes it impossible to realize the rapid assembly and mass production of small satellites

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
  • Architecture for supporting ultrahigh power consumption of small satellite
  • Architecture for supporting ultrahigh power consumption of small satellite
  • Architecture for supporting ultrahigh power consumption of small satellite

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the drawings in the embodiments of the present invention.

[0014] see Figure 1 to Figure 2 , the embodiment of the present invention provides an architecture 100 supporting ultra-high power consumption of a small satellite S, the architecture 100 may include:

[0015] Main structure 110, see specifically figure 2 , the main structure 110 is formed with a plurality of compartments 111 for installing the satellite unit U of the small satellite S, and the plurality of compartments 111 are distributed in the same distribution plane P, wherein figure 2 The grid-like main structure 110 is exemplarily shown in , where the 18 "grids" are the 18 compartments 111 of the main structure 110, as figure 2 As shown, these compartments 111 are distributed in the main structure 110 in the form of a two-dimensional matrix. In other words, these c...

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

PropertyMeasurementUnit
Thicknessaaaaaaaaaa
Login to view more

Abstract

The embodiment of the invention discloses an architecture for supporting ultrahigh power consumption of a small satellite. The architecture comprises a main body structure, an attitude control cabin and a solar panel, wherein the main body structure is provided with a plurality of cabin segments for installing a satellite single unit of the small satellite, and the plurality of cabin segments aredistributed in the same distribution plane; the attitude control cabin is arranged in the distribution plane where the cabin segments are distributed so that the main body structure and the attitude control cabin are integrally in a plate shape; and the solar panel is configured to be in an unfolded state extending out of the main body structure so as to convert solar energy into electric energy used by the small satellite.

Description

technical field [0001] The invention relates to the field of overall configuration design of small satellites, in particular to a structure supporting ultra-high power consumption of small satellites. Background technique [0002] With the continuous development of small satellite technology, the satellite load in the small satellite needs higher and higher total power to achieve higher satellite performance. At the same time, the high power of the load will cause the small satellite to generate more heat. Take communication-type small satellites as an example. The weight of such small satellites is usually about 200kg, and the long-term power consumption in orbit will reach the kilowatt level. Due to the high long-term power consumption in orbit, a large amount of heat will be generated. [0003] The overall structure of the current small satellite is usually in the shape of a cube. In order to dissipate the heat generated by the small satellite, it is usually necessary to ...

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
IPC IPC(8): G06F30/17G06F119/08
CPCG06F30/17G06F2119/08Y02E10/50
Inventor 郭金生李化义曹喜滨张冀鹞
Owner HARBIN INST OF TECH
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