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Basic data
| Standard ID | GB/T 44776-2024 (GB/T44776-2024) |
| Description (Translated English) | General requirements of simulation analysis for space environments and their effects on spacecraft |
| Sector / Industry | National Standard (Recommended) |
| Classification of Chinese Standard | V06 |
| Classification of International Standard | 49.020 |
| Word Count Estimation | 87,859 |
| Date of Issue | 2024-10-26 |
| Date of Implementation | 2024-10-26 |
| Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration |
GB/T 44776-2024: General requirements of simulation analysis for space environments and their effects on spacecraft
---This is an excerpt. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.), auto-downloaded/delivered in 9 seconds, can be purchased online: https://www.ChineseStandard.net/PDF.aspx/GBT44776-2024
ICS 49.020
CCSV06
National Standard of the People's Republic of China
Spacecraft space environment and its effects
General requirements for simulation analysis
Released on October 26, 2024
Implementation on October 26, 2024
State Administration for Market Regulation
The National Standardization Administration issued
Table of Contents
Preface III
1 Scope 1
2 Normative references 1
3 Terms and Definitions 1
4 Abbreviations 3
5 General process of simulation analysis of space environment and its effects 4
6 Task Analysis Requirements 6
7 Requirements for analysis of spatial environment and its effect factors 6
8 Requirements for analysis of space environment and its effect parameters 8
8.1 Vacuum and Outgassing Effect Parameter Analysis 8
8.2 Analysis of temperature environment and its effect parameters 9
8.3 Analysis of atmospheric environment and its effect parameters 9
8.4 Analysis of Space Radiation Environment and Its Effect Parameters 9
8.5 Analysis of Solar Electromagnetic Radiation Environment and Its Effect Parameters 10
8.6 Analysis of Plasma Environment and Its Effect Parameters 10
8.7 Analysis of Space Magnetic Field Environment and Its Effect Parameters 10
8.8 Analysis of Space Debris and Micrometeoroid Environment and Its Effect Parameters 10
8.9 Analysis of dust and dust storm environment and its effect parameters 10
9 Solar Activity Analysis Requirements 11
9.1 Analysis of Medium- and Long-Term Solar Activity 11
9.2 Analysis of Short-Term Solar Eruptive Activity 11
10 Requirements for planetary magnetic field impact analysis 11
11 Track Analysis and Modeling Requirements11
11.1 Orbital Analysis 11
11.2 Track Modeling 11
12 Spacecraft Structural Analysis and Modeling Requirements 11
12.1 Spacecraft Structural Analysis 11
12.2 Spacecraft Structural Modeling 12
13 Space Environment Simulation Analysis 12
13.1 General requirements 12
13.2 Spatial Environment Model 12
13.3 Principles for selecting spatial environment models 14
14 Requirements for simulation analysis of space environment and its effects 15
14.1 General requirements 15
14.2 Simulation Analysis of Vacuum Outgassing Effect 15
14.3 Simulation Analysis of Spacecraft Thermal Environment Effects 16
14.4 Simulation Analysis of Atmospheric Environmental Effects 16
14.5 Single Event Effect Simulation Analysis 17
14.6 Simulation Analysis of Total Ionization Dose Effect 18
14.7 Simulation Analysis of Displacement Damage Effects 19
14.8 Simulation Analysis of Solar Electromagnetic Radiation Effects 19
14.9 Simulation Analysis of Surface Charge and Discharge Effects 19
14.10 Simulation Analysis of Deep Charging/Internal Charging Effects 20
14.11 Simulation Analysis of Space Magnetic Field Effects 20
14.12 Simulation Analysis of Space Debris and Meteoroid Impact Effects 21
14.13 Simulation Analysis of Dust and Dust Storm Effects 22
15 Result output requirements 22
15.1 Track Display 22
15.2 Data Output 22
15.3 Image and Video Output 22
Appendix A (Normative) Geomagnetic Cutoff Stiffness 24
Appendix B (Normative) IGRF Model 26
Appendix C (Informative) Commonly used space environment effect analysis software and codes 28
Appendix D (Informative) Brief Introduction to the Main Space Environment Models 32
Appendix E (Informative) Fick Diffusion Theory of Molecular Outgassing Pollution 37
Appendix F (Normative) Molecular Contamination Transmission Angle Coefficient Method 39
Appendix G (Informative) Molecular Contamination Adhesion Coefficient Model 40
Appendix H (Normative) Neutral Atmosphere Drag on Spacecraft 42
Appendix I (Informative) Key Parameters of Neutral Atmosphere Physical Sputtering 43
Appendix J (Normative) Single Event Effects Prediction Method 44
Appendix K (Normative) Shielding Simulation Analysis Method 47
Appendix L (Informative) Radiation Dose Analysis Method 51
Appendix M (Informative) Displacement Damage Effect Analysis Method 53
Appendix N (Normative) Calculation Method of Insolation Factor and Light Geometric Factor 56
Appendix O (Informative) General Process for Simulation Analysis of Surface Charge and Discharge Effects 58
Appendix P (Informative) Spacecraft Surface Charging Mechanism 59
Appendix Q (Informative) General Process for Simulation Analysis of Deep Charging/Internal Charging Effects 61
Appendix R (Informative) Spacecraft Internal Charging Mechanism 62
Appendix S (Normative) Calculation of Spacecraft Magnetic Interference Torque 66
Appendix T (Informative) Commonly Used Ballistic Limit Equations 67
Appendix U (Normative) PNI and PNP Calculation Methods 71
Appendix V (Informative) Prediction Model of Optical Performance Degradation Caused by Accumulative Impact Damage 73
Appendix W (Informative) Lunar Dust Shielding Effect Model 75
Reference 77
Preface
This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for standardization work Part 1.Structure and drafting rules for standardization documents"
Drafting.
Please note that some of the contents of this document may involve patents. The issuing organization of this document does not assume the responsibility for identifying patents.
This document was proposed by the Chinese Academy of Sciences.
This document is under the jurisdiction of the National Technical Committee for Standardization of Aerospace Technology and Its Applications (SAC/TC425).
This document was drafted by. Beijing Satellite Environmental Engineering Research Institute, Shenzhen Star Earth Twin Technology Co., Ltd., Harbin Institute of Technology, China Academy of Sciences
National Space Science Center, Beijing Spacecraft General Design Department, Xiangtan University, Nanjing University of Aeronautics and Astronautics, China Space Technology Research Institute
Institute of Physics and Chemistry, Chinese Academy of Sciences, Xinjiang Institute of Physics and Chemistry, Xi'an Jiaotong University, Beijing Weidong Space-Time Technology Co., Ltd., Zhongke Xingtu Measurement and Control Technology Co., Ltd.
Co., Ltd., Xi'an Longfei Electric Technology Co., Ltd., Space Application Engineering and Technology Center of the Chinese Academy of Sciences, Digital Space (Beijing) Technology
Joint-stock company, Harbin Institute of Technology Satellite Technology Co., Ltd.
The main drafters of this document are. Shen Zicai, Ji Qizheng, Ouyang Xiaoping, Li Xingji, Cai Minghui, Wang Shijin, Tang Xiaobin, Xiang Yanchao, Qu Shaojie,
Qiu Zhenyu, Hu Yanqi, Mei Bo, Li Yudong, Fang Meihua, Chen Yu, Cao Yan, Chen Jingang, Chen Yupeng, Luo Dan, Zhang Xin, Li Changhong, Wang Xinyue, Yang Jianqun,
Jiao Zilong, Mao Xin, Guo Qi, Tang Xiaojun, Zhang Yuanyuan, Liu Yenan, Ding Yigang, Ma Xin, Dai Wei, Wang Hanfeng, Ren Siyuan, Chen Jian, Sun Wei, and Liu Wei.
Spacecraft space environment and its effects
General requirements for simulation analysis
1 Scope
This document specifies the general requirements for spacecraft space environment and its effects simulation analysis, including the space environment and its effects simulation analysis
General process, mission analysis, space environment and its effect factor analysis, space environment and its effect parameter analysis, solar activity analysis, planetary magnetism
Field impact analysis, orbit analysis and modeling, spacecraft structure analysis and modeling, space environment simulation analysis, space environment and its effects simulation analysis
analysis, simulation analysis result output and other requirements.
This document applies to spacecraft and its materials, components, assemblies, etc. in vacuum, charged particles, ultraviolet radiation, neutral atmosphere (including atomic oxygen),
Plasma, pollution, micrometeoroids and space debris, dust and dust storms and other environments and their single particle effects, total ionization dose effects, displacement damage effects
Effects of surface charge and discharge, deep charge/internal charge, atomic oxygen erosion, micrometeoroid and space debris impact, and contamination
It is also applicable to the design and development of simulation analysis software and codes for spacecraft space environment and its effects, as well as the space environment of organisms.
It is used as a reference for analysis of the space environment and its effects.
2 Normative references
The contents of the following documents constitute the essential clauses of this document through normative references in this document.
For referenced documents without a date, only the version corresponding to that date applies to this document; for referenced documents without a date, the latest version (including all amendments) applies to
This document.
GB/T 29079 Spacecraft orbit classification and common parameter symbols
GB/T 30114.2 Terminology of Space Science and Its Applications Part 2.Space Physics
GB/T 32452 Spacecraft Space Environment Terminology
GB/T 37834 Galactic cosmic ray model
GB/T 41214 Prediction methods for geomagnetic activity in space environments (natural and artificial)
GB/T 41457 Space environment - Geosynchronous orbit solar proton flux and its statistical model confidence level selection guide
GB/T 41458 Space environment. Plasma environment that produces the worst potential difference on the surface of a spacecraft
GB/T 41459 Space environment - Total solar irradiance
GB/T 42214 Space environment low altitude (300km~600km) high energy radiation model
GB/T 42242 Assessment of radiation effects of commercial off-the-shelf (COTS) components used in low-orbit satellites in the space environment
GB /Z 42244 Procedure for obtaining worst-case scenarios and confidence levels for the Earth's radiation belt flux using a quasi-dynamic model of the space environment
GB/T 42846 Ground simulation method for space radiation effects of non-metallic materials in space environment
GB/T 44001 Space environment geomagnetic field reference model
GB /Z 44002 Method for determining proton flux and peak flux of solar energy in space environment
GB/T 44181 Method for predicting the single event upset rate of aerospace semiconductor devices in space environment
3 Terms and Definitions
The terms and definitions defined in GB/T 29079, GB/T 30114.2 and GB/T 32452 and the following terms and definitions apply to this document.
...