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GB/T 38190-2019 English PDF

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GB/T 38190-2019: Test method of electron irradiation aerospace solar cells
Status: Valid
Standard IDUSDBUY PDFLead-DaysStandard Title (Description)Status
GB/T 38190-2019199 Add to Cart 3 days Test method of electron irradiation aerospace solar cells Valid

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Basic data

Standard ID: GB/T 38190-2019 (GB/T38190-2019)
Description (Translated English): Test method of electron irradiation aerospace solar cells
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: F12;V76
Classification of International Standard: 27.160; 49.140
Word Count Estimation: 10,123
Date of Issue: 2019-10-18
Date of Implementation: 2020-05-01
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration

GB/T 38190-2019: Test method of electron irradiation aerospace solar cells

---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.
Test method of electron irradiation aerospace solar cells ICS 27.160; 49.140 F12; V76 National Standards of People's Republic of China Aerospace solar cell electron irradiation test method Published on.2019-10-18 2020-05-01 implementation State market supervision and administration China National Standardization Administration issued

Foreword

This standard was drafted in accordance with the rules given in GB/T 1.1-2009. This standard is proposed and managed by the National Aerospace Technology and its Application Standardization Technical Committee (SAC/TC425). This standard was drafted. Shanghai Space Power Research Institute, Xinjiang Institute of Physics and Technology. The main drafters of this standard. Yang Hongdong, Yang Guang, Jiang Depeng, Lei Gang, Lu Jianfeng, Guo Qi, Chen Guoling, Yan, Wang Zhibin, Fan Wei, Maria Henny, Tan Xueyan. Aerospace solar cell electron irradiation test method

1 Scope

This standard specifies the equipment, test and test items, test and test for ground-based simulated electron beam irradiation test for aerospace solar cells. Procedures, trial interruptions and processing, reporting and recording. This standard applies to aerospace solar cells, including monocrystalline silicon solar cells, germanium-based single-junction gallium arsenide solar cells, germanium-based triple-junction gallium arsenide Electron irradiation of solar cells, flip-chip triple-arsenide solar cells, flip-chip four-junction gallium arsenide solar cells, and other types of space solar cells test.

2 Normative references

The following documents are indispensable for the application of this document. For dated references, only dated versions apply to this article. Pieces. For undated references, the latest edition (including all amendments) applies to this document. GB/T 2297-1989 Solar photovoltaic energy system terminology GB/T 6494 Aerospace solar cell electrical performance test method GB/T 6495.4 Temperature and irradiance correction method for IV measured characteristics of crystalline silicon photovoltaic devices GB/T 6495.9-2006 Photovoltaic devices - Part 9. Performance requirements for solar simulators GB/T 6496-2017 Aerospace solar cell calibration method ISO 15387 Space System Single Junction Solar Cell Measurement and Calibration Procedure (Spacesystems-Single-junctionsolar cels-Measurementsandcalibrationprocedures)

3 Terms and definitions

The following terms and definitions as defined in GB/T 2297-1989 apply to this document. 3.1 Flux rate The number of particles passing through the unit area per unit time. Note. The unit is electrons per square centimeter second [e/(cm2·s)]. 3.2 Fluence The number of particles injected per unit area over a period of time. Note 1. The unit is electron per square centimeter (e/cm2). Note 2. It can also be regarded as the integral of the fluence rate with time.

4 Test purposes

Through the electronic radiation test of aerospace solar cells, the ground unit simulation test data is provided for the user unit, and the aerospace solar cell is evaluated. Adaptability in a space-charged particle irradiation environment.
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