GB/T 41542-2022 English PDF

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GB/T 41542-2022: General specification of observation elements for Earth orbit environment
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Basic data

Standard ID: GB/T 41542-2022 (GB/T41542-2022)
Description (Translated English): General specification of observation elements for Earth orbit environment
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V75
Word Count Estimation: 10,155
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration

GB/T 41542-2022: General specification of observation elements for Earth orbit environment

---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
General specification of observation elements for Earth orbit environment ICS 49.090 CCSV75 National Standards of People's Republic of China General Specification for Elements of Earth Satellite Orbit Space Environment Detection Published on 2022-07-01 2023-02-01 Implementation State Administration for Market Regulation Released by the National Standardization Administration directory Preface I 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Detection object 2 5 Technical requirements for detection elements 2 5.1 Neutral atmosphere sounding elements 2 5.2 Elements of ionospheric plasma detection 2 5.3 Magnetospheric Plasma Detection Element 3 5.4 Radiation belts and solar cosmic ray high-energy charged particle detection elements 3 5.5 Elements of Solar X-ray Detection 3 5.6 Near-Earth Space Electromagnetic Field Detection Elements 4 6 Detection method 4 Reference 6

foreword

This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for Standardization Work Part 1.Structure and Drafting Rules of Standardization Documents" drafted. Please note that some content of this document may be patented. The issuing agency of this document assumes no responsibility for identifying patents. This document is proposed by the Chinese Academy of Sciences. This document is under the jurisdiction of the National Technical Committee for Standardization of Space Science and Its Applications (SAC/TC312). This document is drafted by. National Space Science Center, Chinese Academy of Sciences. The main drafters of this document. Wang Xinyue, Chen Tao, Li Zhitao, Zhou Bin, Wang Chunqin, Guan Yibing, Wei Fei, Kong Linggao, Sun Yueqiang, Zhang Aibing, Jing Tao. General Specification for Elements of Earth Satellite Orbit Space Environment Detection

1 Scope

This document specifies the technical requirements for the detection objects and detection elements for in-situ space environment detection in the earth satellite orbit. On-orbit detection method for detection elements. This document is applicable to the in-situ space environment detection payload of the earth satellite orbit with an orbital altitude of.200km~36000km from the earth The configuration, design and application of other spacecraft are implemented by reference.

2 Normative references

There are no normative references in this document.

3 Terms and Definitions

The following terms and definitions apply to this document. 3.1 low earth orbit lowearthorbit; LEO A satellite orbit with an orbital altitude below.2000km from the Earth's surface. 3.2 sun-synchronous orbit; SSO The angular velocity of satellite orbital plane precession is the same orbital velocity as the plane of the sun moves at the equator. 3.3 middle earth orbit; MEO The orbital altitude is between.2000km and.20000km from the earth's surface. 3.4 geosynchronous orbit; GEO The orbital period is equal to the rotation period of the earth, and the orbital height is about 36000km from the earth's surface to the prograde satellite orbit. 3.5 A geosynchronous orbit with an orbital inclination not equal to 0°. Note. The sub-satellite point trajectory of the satellite running on this orbit is a closed curve in the shape of an "8". 3.6 geostationary orbit A geosynchronous orbit with an orbital inclination of 0°. Note. The position of the satellite operating in this orbit relative to the ground remains unchanged. 3.7 Neutral Atmosphere A non-ionized gas in the Earth's atmosphere. ......

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