标准编号：ISO 16127:2014
中文名称：空间系统 无人飞船的解体预防
英文名称：Space systems — Prevention of break-up of unmanned spacecraft
发布日期：2014-02
标准范围
This International Standard defines the requirements to reduce the risk of in-orbit break-up ofunmanned spacecraft, both during and after their operational lives. The aim would be met by reducingthe possibility of a break-up caused by an unplanned internally caused event and by depleting to a safelevel all the sources of stored energy at the end of a spacecraft’s life. This International Standard isdesigned for use in planning, verifying, and implementing the prevention of break-up of a spacecraft.This International Standard applies only to unmanned spacecraft operating in Earth orbit. It does notapply to manned space vehicles or launch vehicle orbital stages. Additionally, it does not cover nuclearpower sources within spacecraft.This International Standard is not applicable to fragmentation as a result of external particle impacts(which includes fragmentations triggered by external particle impact but powered by internal energysources).
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