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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