GB/T 38314-2019
ActiveLithium ion battery design and verification requirements for space application
宇航用锂离子蓄电池组设计与验证要求
Application Summary AI generated
This standard specifies the design, testing, and verification requirements for lithium-ion battery packs used in spacecraft, including satellites and launch vehicles. It covers performance criteria such as charge/discharge cycles, thermal management, and safety under vacuum and microgravity conditions. The standard is applied by aerospace manufacturers and testing agencies to ensure battery reliability and mission safety in orbital and deep-space environments.
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.