GB/T 40536-2021
ActiveDesign requirements for residual propellant venting of Spacecraft
航天器剩余推进剂排放设计要求
Application Summary AI generated
This standard specifies the design requirements for safely venting residual propellant from spacecraft after mission completion or during disposal phases. It is applied in the aerospace industry for the design, testing, and operation of spacecraft propulsion systems to prevent explosion risks and contamination in orbit. The standard ensures compliance with space debris mitigation guidelines and is used by engineers and procurement professionals for spacecraft development and qualification.
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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.