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GB/T 32308-2015: Requirements for post-mission disposal of GEO satellites
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| GB/T 32308-2015 | English | 128 |
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Requirements for post-mission disposal of GEO satellites
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GB/T 32308-2015
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Basic data | Standard ID | GB/T 32308-2015 (GB/T32308-2015) | | Description (Translated English) | Requirements for post-mission disposal of GEO satellites | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V71 | | Classification of International Standard | 49.020 | | Word Count Estimation | 19,155 | | Date of Issue | 2015-12-31 | | Date of Implementation | 2016-07-01 | | Adopted Standard | ISO 26872-2010, NEQ | | Regulation (derived from) | State Standard Announcement 2015 No.43 | | Issuing agency(ies) | General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China | | Summary | This standard specifies requirements for post-mission disposal of GEO satellites, including post-mission departure and deactivation requirements, specific implementation, and documentation requirements. This standard applies to the disposal of GEO satellite after the implementation of the task, other geostationary orbit (GSO) satellite post-processing can refer to the implementation. | GB/T 32308-2015: Requirements for post-mission disposal of GEO satellites---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.
Requirements for post-mission disposal of GEO satellites
ICS 49.020
V71
National Standards of People's Republic of China
GEO satellite mission postponement requirements
(ISO 26872..2010 Spacesystems-Disposalofsatelites
operatingatgeosynchronousaltitude, NEQ)
2015-12-31 released
2016-07-01 implementation
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
China National Standardization Management Committee released
Foreword
This standard is drafted in accordance with the rules given in GB/T 1.1-2009.
This standard uses the re-drafting method for reference to ISO 26872..2010 "Space systems operating at the geosynchronous orbit height of satellite disposal"
Compile, consistent with ISO 26872..2010 is not equivalent.
This standard is proposed by China Aerospace Science and Technology Corporation.
This standard is nationalized by the National Aeronautical Technology and Its Application Standardization Technical Committee (SAC/TC425).
The drafting unit of this standard. China Space Technology Research Institute Communications Satellite Division.
The main drafters of this standard. by Yao Xiang, Liu Jian Gong, Hou Fen, Weng Jia, Zhang Xiangyan, Yang Lingxuan, Wei Xin, Song Tao, Liu Jiang, Tong Jincheng,
Wu Yuxiang.
GEO satellite mission postponement requirements
1 Scope
This standard specifies GEO satellite mission post-processing requirements, including post-mission off-track and passivation requirements, implementation and documentation
Waiting for.
This standard applies to the disposal of GEO satellites (hereinafter referred to as satellites), and other geosynchronous orbit (GSO) satellites
Post-processing can refer to the implementation.
2 terms and definitions
The following terms and definitions apply to this document.
2.1
Post-missiondisposal post-missiondisposal
After the end of the actual mission of the satellite, in order to protect the space environment and to avoid harm to other satellites in orbit, and take away from the rail operation and passivation
Measures.
2.2
Earth Synchronous Track geosynchronousearthorbit; GSO
The orbital period is equal to the Earth's rotation cycle.
2.3
Geostationary geostationary geostation
A geostationary orbit with an inclination of 0 ° and an eccentricity of zero.
Note. Generally, a geostationary orbit with a small inclination and a small eccentricity is called the geostationary orbit.
2.4
Dispose of the track
For permanent placement of the post-mission satellite area.
2.5
GEO Region GEOregion
Earth geostationary orbit ± 40km, latitude direction ± 0.1 ° area.
2.6
GEO protected area GEOprotectedregion
The geostationary orbit is ±.200km in radial direction and ± 15 ° in the equatorial direction.
Note. GEO protection area shown in Figure 1.
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