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GB/T 46190-2025General requirements of protection for space environmental effects on spacecraft (English PDF)

航天器空间环境效应防护通用要求

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

October 5, 2025

Implementation date

October 5, 2025

Scope

GB/T 46190-2025 is the English-translated version of 航天器空间环境效应防护通用要求.

GB/T 46190-2025 is the Chinese standard "General requirements of protection for space environmental effects on spacecraft".

Its scope clause reads: This document specifies the procedures for protecting spacecraft from the effects of the space environment, including single-event effects, total ionization dose effects, displacement damage effects, and surface effects.

Surface charging and discharging effect, internal charging effect, ultraviolet radiation damage effect, pollution effect, atomic oxygen erosion effect, and impact of space debris and micrometeoroids.

General requirements for protection against the effects. This document applies to the protection of spacecraft products against space environment effects. Its clauses include terms and definitions.

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Document preview — GB/T 46190-2025

National Standard of the People's Republic of China

ICS
49.020
Classification
V 06

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.Basic Requirements
  • 6.Spacecraft Space Environment Effects Protection Workflow
  • 7.Analysis of the spatial environment and its effects
  • 8.Determination of Space Environmental Effect Protection Design Indicators
  • 9.Development of Test Specifications for Spacecraft Space Environment Effects
  • 10 General requirements for protection against single-event effects
  • 11 General requirements for protection against total ionizing dose effects
  • 12 General Requirements for Protection Against Displacement Damage Effects
  • 13 General requirements for protection against surface charge-discharge effects
  • 14 General requirements for protection against internal electric shock effects
  • 15 General Requirements for Protection Against Ultraviolet Radiation Effects
  • 16 General Requirements for Protection Against Atomic Oxygen Erosion Effects
  • 17 General Requirements for Protection Against Space Debris and Micrometeoroid Impacts
  • 18 General Requirements for Pollution Prevention
  • 19 General Requirements for Microgravity Effect Protection
  • 20 Space magnetic field protection requirements
  • 21 Atmospheric and Vacuum Effects Protection Requirements
  • 22 Ionospheric Effect Protection Requirements
  • 23.Protection requirements against micro-vibration effects
  • 24.On-orbit protection against spacecraft space environment effects
  • 25 Other
  • Appendix A (Informative) Classification of Device Radiation Sensitivity
  • Appendix B (Informative) Radiation Design Margin
  • Appendix C (Informative) Design Process for Space Radiation Effect Protection
  • Appendix D (Informative) Methods for Predicting Single-Event Effects
  • Appendix E (Informative) Simple Shielding Analysis Method
  • Appendix F (Informative) Surface Charge and Discharge Risks
  • Appendix G (Informative) Risk of Internal Charge Effect
  • Appendix H (Normative) Vacuum Micro-discharge Test Methods

1 Scope

This document specifies the procedures for protecting spacecraft from the effects of the space environment, including single-event effects, total ionization dose effects, displacement damage effects, and surface effects.

Surface charging and discharging effect, internal charging effect, ultraviolet radiation damage effect, pollution effect, atomic oxygen erosion effect, and impact of space debris and micrometeoroids.

General requirements for protection against the effects.

This document applies to the protection of spacecraft products against space environment effects.

2 Normative references

The contents of the following documents, through normative references within the text, constitute essential provisions of this document. Dated citations are not included.

For references to documents, only the version corresponding to that date applies to this document; for undated references, the latest version (including all amendments) applies.

This document.

GB/T 4937.2 Mechanical and climatic testing methods for semiconductor devices - Part 2.Low pressure

GB/T 30114.2 Terminology for Space Science and Its Applications Part 2.Space Physics

GB/T 32452 Space Terminology - Space Environment

GB/T 34517 Evaluation Method for Vacuum Outgassing of Non-metallic Materials for Spacecraft

GB/T 41543 General Specification for Simulation Test of Space Environment Effects on Space Materials for Space Environment

GB/T 42242 Evaluation of Radiation Effects of Commercial Off-the-Shelf (COTS) Devices Used in Low Earth Orbit Satellites in Space Environment

GB/T 42846-2023 Ground-based simulation method for space radiation effects of non-metallic materials in the space environment

GB/T 44385-2024 General requirements for ensuring the adaptability of spacecraft to the space environment

GB/T 44776 General Requirements for Simulation Analysis of Space Environment and Its Effects of Spacecraft

3 Terms and Definitions

The terms and definitions defined in GB/T 32452, GB/T 30114.2 and GB/T 44385-2024, as well as the following terms and definitions, apply to this document.

3.1

The ratio of the radiation dose that causes a material or device to fail due to radiation to the ambient radiation dose at the actual location of use on the satellite.

3.2 Watchdogtimer;WDT

A timer circuit that uses hardware or software to generate a reset signal and restart the system when a program malfunctions.

3.3 wake effect

When a spacecraft is orbiting in a low-altitude, non-polar Earth orbit, its speed exceeds the speed of sound of ions, causing [the following to occur] within the spacecraft.

The phenomenon of an ion depletion region being formed in the opposite direction of motion.

3.4

During strong solar activity events such as coronal mass ejections, the solar wind compresses the Earth's magnetopause to below the altitude of geosynchronous orbit, leading to...

GB/T 38239 | GB/T 36249 | GB/T 46195 | GB/T 46189 | […]

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 40 pages — is available in the English PDF.

Referenced standards

Editions of GB/T 46190

EditionTitleRevisionStatus
GB/T 46190-2025General requirements of protection for spaceenvironmental effects on spacecraftcurrent editionCurrent

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