本国际标准定义了在试验过程中用于确定荷载和诱导环境的原则 综合考虑概率概念的航天器及其部件的使用寿命 载荷、相应的安全系数和生命周期。

This International Standard defines the principles used to determine loads and the induced environment during the service life of a space flight vehicle and its components, taking account of the notions of probability, combined loads, corresponding safety factors and lifecycle.