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

Space-based large-diameter multi-constrained extrasolar terrestrial planet detector structure

A large-caliber, multi-constraint technology, applied in aircraft, aerospace vehicles, aerospace equipment, etc., can solve the problems of high center of mass of the whole device and difficulty in the overall configuration design of the detector, so as to reduce the center of mass of the whole device and improve the attitude The effect of controlling accuracy and reducing attitude measurement error

Inactive Publication Date: 2017-02-22
SHANGHAI SATELLITE ENG INST
View PDF6 Cites 10 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, due to the large aperture and many constraints of the large space camera, it brings difficulties to the overall configuration design of the detector
According to analysis, in order to realize the detection of exoplanets, the camera needs to have a diameter of 3m, a height of 3.3m, and a rear optical path height of 1.7m. The overall envelope exceeds the limit of the launch vehicle fairing, and the center of mass of the entire vehicle is too high

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
  • Space-based large-diameter multi-constrained extrasolar terrestrial planet detector structure
  • Space-based large-diameter multi-constrained extrasolar terrestrial planet detector structure

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0014] like Figure 1 to Figure 2 As shown, the embodiment of the present invention provides a configuration of a space-based large-aperture multi-constraint exoplanet probe, which is characterized in that it includes a platform service module 1, a platform propulsion module 2, a payload 3, and a star sensor 4 and the platform bottom plate 5, the rear optical path of the payload 3 is embedded in the platform service cabin 1, so as to realize the integrated design of the load platform, reduce the e...

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 space-based large-diameter multi-constrained extrasolar terrestrial planet detector structure. The structure comprises a platform service module, a platform propelling module, a payload, a star sensor and a platform bottom plate; the back light path part of the payload is embedded into the platform service module, the star sensor is installed on a high-rigidity back plate of the payload, therefore, the attitude measuring error is decreased, and the attitude control precision of a whole detector is improved; intra-detector subsystem single units of the detector are arranged on the obverse side of the platform bottom plate, and thrusters and air cylinders are arranged on the reverse side of the platform bottom plate. According to the space-based large-diameter multi-constrained extrasolar terrestrial planet detector structure, by means of integrated design of a load platform, the mass center of the whole detector can be lowered, and the enveloping limiting requirement of a launch vehicle fairing can be met; meanwhile, attitude sensitive devices such as the star sensor are arranged on the high-rigidity back plate of the payload, therefore, the attitude measuring error can be decreased, and the attitude control precision of the whole detector can be improved. The structure can be effectively applied to layout design of a similar detector structure with a large-diameter multi-constrained space camera.

Description

technical field [0001] The invention relates to the configuration of a space-based large-aperture multi-constraint exoplanet probe, which provides a configuration layout scheme for the overall design of the probe, and the configuration layout scheme can be applied to similar large-aperture multiple Detector design for constrained space cameras. Background technique [0002] As a typical detection object, extrasolar terrestrial planets carry the significance of discovering habitable planets and extrasolar life, and are the hotspot and focus of current research. Developing fine spectral measurement technology, launching large-scale space cameras, studying exoplanet atmospheres, and finely characterizing the physical and chemical properties of exoplanets are important directions for future space exploration. [0003] However, due to the large aperture and many constraints of large-scale space cameras, it brings difficulties to the overall configuration design of the detector. ...

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): B64G1/66
CPCB64G1/66
Inventor 黄帆方宝东张嵬张恒饶启龙
Owner SHANGHAI SATELLITE ENG INST
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