17704692435
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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本文件规定了航天运载火箭和航天器用火工系统和装置的火工系统要求、火工装置要求、产品保障要求。本文件适用于航天运载火箭和航天器用火工系统和装置的设计、生产制造、试验验证、贮存使用。
本标准规定了航天器常压热性能试验的试验目的、试验原理、试验要求及试验方法。本标准适用于航天器或其舱段、大型组件常压热性能试验，包括密封舱常压综合热试验、常压热变形试验、常压热环境下的分离与展开试验，其他大型组件热性能试验可参照使用。
This standard specifies the purpose, principle, requirements and method of spacecraft performance test under ambient pressure and thermal environment.
This standard is applicable to the performance tests of spacecraft or its cabin and large assemblies under ambient pressure and thermal environment, including integrated thermal test for sealed cabin, thermal deformation test under ambient pressure, separation and deployment test under ambient pressure and thermal environment, and can serve as a reference for the thermal performance tests of other large assemblies.
本标准规定了微纳卫星产品的机械、热、电气、信号、磁等接口的一般要求与详细要求。
本标准适用于微纳卫星产品的机械、热、电气、信号、磁等接口的设计，微纳卫星载荷产品接口可参照使用。
This standard specifies the general and detailed requirements for mechanical, thermal, electrical, signal and magnetic interfaces of micro-nano satellite equipment.
This standard is applicable to the design of mechanical, thermal, electrical, signal and magnetic interfaces of micro-nano satellite equipment, and can serve as a reference for interfaces of micro-nano satellite payload equipment.
本标准规定了微纳卫星及其组件试验的一般要求、微纳卫星系统级试验、组件级试验和详细要求。
本标准适用于微纳卫星及其组件试验计划的制定与实施。
本标准规定了载人航天周边式对接机构通用对接接口要求，包括机械接口、热接口和载荷要求，浮动断接器和对接性能要求。本标准适用于近地轨道载人航天和国际对接合作等任务的对接机构接口设计，载人登月等其他航天器的对接接口设计可参照使用。
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.
本标准规定了航天器磁性评估和磁性控制的目的、程序和方法。本标准适用于航天器及其部、组件的磁性评估和磁性控制。
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