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GB/T 44776-2024General requirements of simulation analysis for space environments and their effects on spacecraft (English PDF)

航天器空间环境及其效应仿真分析通用要求

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

October 26, 2024

Implementation date

October 26, 2024

Scope

GB/T 44776-2024 is the English-translated version of 航天器空间环境及其效应仿真分析通用要求.

GB/T 44776-2024 is the Chinese standard "General requirements of simulation analysis for space environments and their effects on spacecraft".

Its scope clause reads: 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. Its clauses include terms and definitions.

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Document preview — GB/T 44776-2024

National Standard of the People's Republic of China

ICS
49.020
Classification
V06

Issued by: State Administration for Market Regulation; Standardization Administration of the PRC

Contents

  • Preface
  • 1 Scope
  • 2 Normative references
  • 3 Terms and Definitions
  • 4 Abbreviations
  • 5 General process of simulation analysis of space environment and its effects
  • 6 Task Analysis Requirements
  • 7 Requirements for analysis of spatial environment and its effect factors
  • 8 Requirements for analysis of space environment and its effect parameters
  • 8.1 Vacuum and Outgassing Effect Parameter Analysis
  • 8.2 Analysis of temperature environment and its effect parameters
  • 8.3 Analysis of atmospheric environment and its effect parameters
  • 8.4 Analysis of Space Radiation Environment and Its Effect Parameters
  • 8.5 Analysis of Solar Electromagnetic Radiation Environment and Its Effect Parameters
  • 8.6 Analysis of Plasma Environment and Its Effect Parameters
  • 8.7 Analysis of Space Magnetic Field Environment and Its Effect Parameters
  • 8.8 Analysis of Space Debris and Micrometeoroid Environment and Its Effect Parameters
  • 8.9 Analysis of dust and dust storm environment and its effect parameters
  • 9 Solar Activity Analysis Requirements
  • 9.1 Analysis of Medium- and Long-Term Solar Activity
  • 9.2 Analysis of Short-Term Solar Eruptive Activity
  • 10 Requirements for planetary magnetic field impact analysis
  • 11 Track Analysis and Modeling Requirements
  • 11.1 Orbital Analysis
  • 11.2 Track Modeling
  • 12 Spacecraft Structural Analysis and Modeling Requirements
  • 12.1 Spacecraft Structural Analysis
  • 12.2 Spacecraft Structural Modeling
  • 13 Space Environment Simulation Analysis
  • 13.1 General requirements
  • 13.2 Spatial Environment Model
  • 13.3 Principles for selecting spatial environment models
  • 14 Requirements for simulation analysis of space environment and its effects
  • 14.1 General requirements
  • 14.2 Simulation Analysis of Vacuum Outgassing Effect
  • 14.3 Simulation Analysis of Spacecraft Thermal Environment Effects
  • 14.4 Simulation Analysis of Atmospheric Environmental Effects
  • 14.5 Single Event Effect Simulation Analysis
  • 14.6 Simulation Analysis of Total Ionization Dose Effect
  • 14.7 Simulation Analysis of Displacement Damage Effects
  • 14.8 Simulation Analysis of Solar Electromagnetic Radiation Effects
  • 14.9 Simulation Analysis of Surface Charge and Discharge Effects
  • 14.10 Simulation Analysis of Deep Charging/Internal Charging Effects
  • 14.11 Simulation Analysis of Space Magnetic Field Effects
  • 14.12 Simulation Analysis of Space Debris and Meteoroid Impact Effects
  • 14.13 Simulation Analysis of Dust and Dust Storm Effects
  • 15 Result output requirements
  • 15.1 Track Display
  • 15.2 Data Output
  • 15.3 Image and Video Output
  • Appendix A (Normative) Geomagnetic Cutoff Stiffness
  • Appendix B (Normative) IGRF Model
  • Appendix C (Informative) Commonly used space environment effect analysis software and codes
  • Appendix D (Informative) Brief Introduction to the Main Space Environment Models
  • Appendix E (Informative) Fick Diffusion Theory of Molecular Outgassing Pollution
  • Appendix F (Normative) Molecular Contamination Transmission Angle Coefficient Method
  • Appendix G (Informative) Molecular Contamination Adhesion Coefficient Model
  • Appendix H (Normative) Neutral Atmosphere Drag on Spacecraft
  • Appendix I (Informative) Key Parameters of Neutral Atmosphere Physical Sputtering
  • Appendix J (Normative) Single Event Effects Prediction Method
  • Appendix K (Normative) Shielding Simulation Analysis Method
  • Appendix L (Informative) Radiation Dose Analysis Method
  • Appendix M (Informative) Displacement Damage Effect Analysis Method
  • Appendix N (Normative) Calculation Method of Insolation Factor and Light Geometric Factor
  • Appendix O (Informative) General Process for Simulation Analysis of Surface Charge and Discharge Effects
  • Appendix P (Informative) Spacecraft Surface Charging Mechanism
  • Appendix Q (Informative) General Process for Simulation Analysis of Deep Charging/Internal Charging Effects
  • Appendix R (Informative) Spacecraft Internal Charging Mechanism
  • Appendix S (Normative) Calculation of Spacecraft Magnetic Interference Torque
  • Appendix T (Informative) Commonly Used Ballistic Limit Equations
  • Appendix U (Normative) PNI and PNP Calculation Methods
  • Appendix V (Informative) Prediction Model of Optical Performance Degradation Caused by Accumulative Impact Damage
  • Appendix W (Informative) Lunar Dust Shielding Effect Model

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.

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 81 pages — is available in the English PDF.

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