This standard specifies the general prevention and control requirements for foreign object debris of spacecraft,as well as the prevention and control requirements for foreign object debris of spacecraft in the process of design,assembly,testing,test,packaging,transportation,and operation in launch site (hereinafter referred to as development process).
This standard is applicable to the prevention and control for foreign object debris in the development process of spacecrafts including satellites,spaceships,space stations and space probes,and can serve as a reference for the prevention and control of foreign object debris in the development process of unit products.
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This standard specifies the requirements for universal docking interface of peripheral docking mechanism for manned spacecraft, including requirements for mechanical interface, thermal interface and mechanism load and requirements for umbilical connector and connection performance.
This standard is applicable to interface design of docking mechanism for missions such as Low Earth Orbit (LEO) manned spacecraft, international docking operation, etc.; and can also serve as a reference for the docking interface design of other spacecrafts, such as spacecraft for manned lunar landing, etc.
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This document specifies work items and detailed requirements for space payloads in the ground phase to perform a re-flight mission.
This document is applicable to the re-flight space payload's ground preparation work on space vehicle platforms,such as the retrievable satellite,spacecraft,space lab,space station,and space probe.
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