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GB/T 34511-2017: Relative motion analysis elements after LV/SC separation
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| GB/T 34511-2017 | English | 239 |
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Relative motion analysis elements after LV/SC separation
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GB/T 34511-2017
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Basic data | Standard ID | GB/T 34511-2017 (GB/T34511-2017) | | Description (Translated English) | Relative motion analysis elements after LV/SC separation | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V70 | | Classification of International Standard | 49.020 | | Word Count Estimation | 12,161 | | Date of Issue | 2017-11-01 | | Date of Implementation | 2018-05-01 | | Regulation (derived from) | National Standard Announcement 2017 No. 29 | | 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 34511-2017: Relative motion analysis elements after LV/SC separation---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.
Relative motion analysis elements after LV/SC separation
ICS 49.020
V70
National Standards of People's Republic of China
Star Arrow separation far-field analysis of elements
(ISO 16679.2015, Spacesystems-Relative motion analysis
elementsafterLV/SCseparation, IDT)
Posted.2017-11-01
2018-05-01 implementation
General Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China
China National Standardization Administration released
Foreword
This standard was drafted in accordance with the rules given in GB/T 1.1-2009.
This standard uses the translation method identical with ISO 16679.2015 "Space System Star Arrow separation far-field analysis of elements."
This standard made the following editorial changes.
--- Standard name changed to "Star Arrow separation far-field analysis elements."
This standard proposed by China Aerospace Science and Technology Corporation.
This standard by the National Aerospace Technology and Standardization Technical Committee (SAC/TC425) centralized.
This standard was drafted by Beijing Institute of Aerospace Systems Engineering.
The main drafters of this standard. Song Qiang, Zhou Shuai, Zhu Dong Court, Han Xueying, Tang Liang, Xiao Qing, Liu Yin, Shen An, Xie Xuan.
Introduction
Far-field analysis predicts the relative distance after the separation of the rocket from the spacecraft. Analysis results provide support for task design and operation.
This standard for the carrier rocket and spacecraft operators, manufacturing manufacturers to provide specific elements and processes for the development of satellite separation far-field analyst
Used to regulate common ground and provide guidance.
Star Arrow separation far-field analysis of elements
1 Scope
This standard specifies the Star Arrow separation far-field analysis elements, including the analysis of input, analysis process, analysis principles, analysis methods, analysis of output.
This standard applies to mission design and verification of spacecraft and launch vehicle separation relative motion prediction. This standard involves a single launch
The relative movement of objects involved in the mission does not cover collision avoidance between launching objects and objects in orbit.
2 Normative references
The following documents for the application of this document is essential. For dated references, only the dated version applies to this article
Pieces. For undated references, the latest edition (including all amendments) applies to this document.
ISO 14303 launch vehicle and spacecraft interface (Launch-vehicle-to-spacecraftinterfaces)
3 Terms and definitions
ISO 14303 defines the following terms and definitions apply to this document.
3.1
Star Arrow separation LV/SCseparation
Under the control of the launch vehicle, the spacecraft and the launch vehicle are disconnected from each other.
3.2
Far-field analysis relativemotionanalysis
Predict the relative distance between the spacecraft (s) and the object (satellites and other objects produced during the separation) after the separation of the stars and arrows
analysis.
3.3
Separation speed separationvelocity
The relative speed between spacecraft and launch vehicle when separation is completed instantly.
4 Abbreviations
The following abbreviations apply to this document.
LV. Launch Vehicle (LaunchVehicle)
SC. Spacecraft
5 Analysis input
The analysis input should include the following information.
a) The theoretical speed, position and attitude of the rocket and (each) spacecraft at the separation point of the star and arrow should be given in a pre-determined coordinate system.
The velocity, position vector should be given in the form of Vx, Vy, Vz, X, Y, Z. For the coordinate systems that may be involved, see Appendix C;
b) speed of separation, body mass and inertia characteristics;
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