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GB/T 38313-2019 English PDF

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GB/T 38313-2019: Design and verification requirements of fibre optic components for space application
Status: Valid

Standard ID	Contents [version]	USD	STEP2	[PDF] delivered in	Standard Title (Description)	Status	PDF
GB/T 38313-2019	English	279	Add to Cart	3 days [Need to translate]	Design and verification requirements of fibre optic components for space application	Valid	GB/T 38313-2019

PDF similar to GB/T 38313-2019

Standard similar to GB/T 38313-2019

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Basic data

Standard ID	GB/T 38313-2019 (GB/T38313-2019)
Description (Translated English)	Design and verification requirements of fibre optic components for space application
Sector / Industry	National Standard (Recommended)
Classification of Chinese Standard	V25
Classification of International Standard	49.035
Word Count Estimation	14,180
Date of Issue	2019-12-10
Date of Implementation	2020-07-01
Issuing agency(ies)	State Administration for Market Regulation, China National Standardization Administration

GB/T 38313-2019: Design and verification requirements of fibre optic components for space application

---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.
Design and verification requirements of fibre optic components for space application ICS 49.035 V25 National Standards of People's Republic of China Design and verification requirements for aerospace fiber optics application 2019-12-10 release 2020-07-01 implementation State Administration of Market Supervision Published by the National Standardization Management Committee

Foreword I 1 Scope 1 2 Normative references 1 3 Terms, definitions and abbreviations 1 3.1 Terms and definitions 1 3.2 Abbreviations 2 4 General requirements 2 4.1 Design Guidelines 2 4.2 Design and development inputs 3 4.3 Design and development output 3 4.4 Design Process 3 5 Design requirements 4 5.1 Functional parameter design 4 5.2 Structural design 5 5.3 Package Design 7 5.4 Thermal Design 7 5.5 Antistatic Design 7 5.6 Anti-radiation design 8 5.7 Reliability Design 8 5.8 Security requirements 8 5.9 Process requirements 8 6 Verification requirements 9 6.1 Function and parameter verification 9 6.2 Environmental adaptability verification 9 6.3 Reliability Verification 10 6.4 Maturity Verification 11 6.5 Application Verification 11

Foreword

This standard was drafted in accordance with the rules given in GB/T 1.1-2009. Please note that some elements of this document may involve patents. The issuer of this document is not responsible for identifying these patents. This standard is proposed and managed by the National Aerospace Technology and Application Standardization Technical Committee (SAC/TC425). This standard was drafted. Beijing Aerospace Times Optoelectronics Technology Co., Ltd. The main drafters of this standard. Liu Jianchun, Zhang Zhixin, Shan Lianjie, Ding Dongfa, Zhang Bingxin, Xiang Yanrong, Wang Cun. Design and verification requirements for aerospace fiber optics

1 Scope

This standard specifies the functional parameters, structure, packaging, and other design and verification of functions, parameters, and reliability of fiber optic devices for aerospace Claim. This standard applies to the process control and selection of aerospace fiber optic device design and verification. Applications in other fields can be implemented by reference.

2 Normative references

The following documents are essential for the application of this document. For dated references, only the dated version applies to this article Pieces. For undated references, the latest version (including all amendments) applies to this document. GB/T 7826-2012 System Reliability Analysis Technology Failure Mode and Impact Analysis (FMEA) Procedure GB/T 14733.12-2008 telecommunication term fiber optic communication ISO 14621-1 Space system power, electronics, electromagnetic components-Part 1. Management [Spacesystems-Electrical, elec- tronicandelectromechanical (EEE) parts-Part 1. Partsmanagement] ISO 14621-2 Space systems, electrical, electronic, and electromagnetic components. Part 2. Requirements for control procedures [Spacesystems-Elec- trical, electronicandelectromechanical (EEE) parts-Part 2. Controlprogramerequirements] 3 Terms, definitions and abbreviations 3.1 Terms and definitions The terms and definitions defined in GB/T 14733.12-2008 and the following apply to this document. 3.1.1 Fiberoptic component Components that work based on the characteristics of the optical fiber or work through discrete components coupled with the optical fiber. Output. Including active fiber optics and passive fiber optics. 3.1.2 Passive fiber optics passivefibreopticcomponent Fiber optics capable of performing certain optical functions by themselves without the aid of any external light or electrical energy, including fiber optic connections , Fiber coupler/beam splitter, wavelength division multiplexer, fiber attenuator, fiber filter, fiber isolator, circulator, polarization controller, fiber Delay lines, fiber gratings, etc. 3.1.3 Activefibreopticcomponent Fiber optic devices that need external energy to drive work that can convert electrical signals into optical signals or convert optical signals into electrical signals, Including semiconductor light sources (LD, LED, DFB, QW, SQW, VCSEL), semiconductor light detectors (PD, PIN, APD), fiber laser, Optical amplifier, wavelength converter, optical modulator, optical switch, etc. 3.1.4 Spacefibreopticsub-system Space systems equipped with fiber optics can perform certain independent functions, including fiber optic sensing systems and fiber optic communication systems.

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