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GB/T 32296-2015: General coordinates for space vehicle
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| GB/T 32296-2015 | English | 128 |
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General coordinates for space vehicle
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GB/T 32296-2015
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Basic data | Standard ID | GB/T 32296-2015 (GB/T32296-2015) | | Description (Translated English) | General coordinates for space vehicle | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V70 | | Classification of International Standard | 49.020 | | Word Count Estimation | 31,343 | | Date of Issue | 2015-12-31 | | Date of Implementation | 2016-07-01 | | 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 | GB/T 32296-2015: General coordinates for space vehicle---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 coordinates for space vehicle
ICS 49.020
V70
National Standards of People's Republic of China
Spacecraft commonly used coordinate system
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 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 of this standard. Beijing Aerospace Systems Engineering Research Institute.
The main drafters of this standard. Li Pingqi, He Wei, Geng Guangyou, Wang Jianming, Chang Wuquan, Ma Ying, Xie Xuan, He Zhaowei, Tian Jichao, Liu Xinglong,
Li Chongyuan.
Spacecraft commonly used coordinate system
1 Scope
This standard specifies the commonly used coordinate systems, definitions, general requirements and transformation formulas for spacecraft.
This standard applies to the overall design of spacecraft such as launch vehicles and spacecraft and interface coordination between systems.
2 normative reference documents
The following documents are indispensable for the application of this document. For dated references, only the dated edition applies to this article
Pieces. For undated references, the latest edition (including all modifications) applies to this document.
GB/T 32455 Carrier Terminology
3 terms and definitions
GB/T 32455 Definitions and the following terms and definitions apply to this document. For ease of use, the following is repeated
Some terms and definitions in GB/T 32455.
3.1
Spacecraft spacevehicle
Perform an aircraft that explores, develops, or utilizes specific tasks such as space.
Note. Spacecraft is divided into transport aircraft (such as launch vehicles) and application aircraft (also known as spacecraft).
3.2
Carrier rocket launchvehicle;
From the surface of the earth, the air will be paid into the space orbit of the rocket.
Note. generally according to the size of the size can be divided into small, medium, large and heavy carrier rocket, near-Earth orbit carrying capacity of 2t and below the launch vehicle for small transport
Rocket, near-Earth orbit carrying capacity 2t ~ 20t carrier rocket for medium-sized carrier rocket, near-Earth orbit carrying capacity 20t ~ 50t carrier rocket
Large launch vehicle, near-Earth orbit carrying capacity of 50t and above the launch vehicle for heavy-duty launch vehicle.
[GB/T 32455, definition 2.1.2]
3.3
Spacecraft spacecraft
In the universe outside the space, the implementation of exploration, development or use of space and other specific tasks of the aircraft. Such as artificial earth satellites
Human spacecraft, space detectors and so on.
3.4
Escape the aircraft escapevehicle
In the event of a fatal fault, the aircraft is separated from the rocket and fled the dangerous area.
3.5
Celestial sphere
An imaginary sphere introduced to determine the position of the celestial body.
Note 1. According to the selected celestial sphere center, there are crescent days, geocentric celestial sphere and so on.
Note 2. The radius of the celestial sphere is arbitrarily selected and can be regarded as mathematically infinite.
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