GB/T 38313-2019
ActiveDesign and verification requirements of fibre optic components for space application
宇航用纤维光学器件设计与验证要求
Application Summary AI generated
This standard specifies the design, manufacturing, and verification requirements for fibre optic components used in spacecraft and satellite systems. It is applied in the aerospace industry to ensure the reliability and performance of optical components under harsh space conditions, including radiation, vacuum, and extreme temperature fluctuations. The standard guides engineers in qualifying components for communication, sensing, and data transmission subsystems in space missions.
Related Standards
GB/T 28878.1-2012
Specification of the rotating component in space science experiments - Part 1：General requirements of design
GB/T 28878.8-2016
Specification of the rotating component in space science experiments—Part 8：Assemble
GB/T 28878.7-2016
Specification of the rotating component in space science experiments—Part 7：Reliability test
GB/T 28878.5-2016
Specification of the rotating component in space science experiments—Part 5: Motors acceptance
GB/T 28878.4-2016
Specification of the rotating component in space science experiments—Part 4：Lubrication oil acceptance
GB/T 28878.3-2016
Specification of the rotating component in space science experiments—Part 3：Ball bearing acceptance
GB/T 28878.2-2016
Specification of the rotating component in space science experiments—Part 2: Requirements of lubrication design
GB/T 28878.6-2016
Specification of the rotating component in space science experiments—Part 6：Property testing
Transparency note: The application summary and key sentences on this page were automatically generated by AI from the standard's original text. This content has not been human-verified and should not be used for compliance or regulatory purposes. Always refer to the official standard document from the issuing authority.