ISO 19683:2017 空间系统 小型航天器和单元的设计资格和验收试验

标准编号：ISO 19683:2017

中文名称：空间系统 小型航天器和单元的设计资格和验收试验

英文名称：Space systems — Design qualification and acceptance tests of small spacecraft and units

发布日期：2017-07

标准范围

ISO 19683:2017规定了小型航天器或装置的设计鉴定和/或验收的试验方法和试验要求。它提供了最低测试要求和测试方法，以确认商用小型航天器及其组件的设计和制造方法，并接受最终产品。ISO 19683:2017强调了在保持低成本和快速交付的同时，实现卫星发射入轨后婴儿死亡率的可靠性。如图1所示，ISO 19683:2017适用于其开发方法不同于风险承受能力较小的传统卫星的开发方法的卫星。本文件的范围包括不同类别的小型航天器，即所谓的微型、微型、纳米、皮科和飞秒级航天器，以及立方体卫星航天器。因此，为了方便起见，本文件通篇使用“小型航天器”作为通用术语。ISO 19683:2017包括CubeSat，只要它是用非传统工艺开发的。

ISO 19683:2017 provides test methods and test requirements for design qualification and/or acceptance of small spacecraft or units. It provides the minimum test requirements and test methods to qualify the design and manufacturing methods of commercial small spacecraft and their units and to accept the final products.

ISO 19683:2017 places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low cost and fast delivery.

ISO 19683:2017 is applied to satellites whose development methods are different from the ones used for traditional satellites that have little room for risk tolerance, as shown in Figure 1. The scope of this document encompasses different categories of small spacecraft, so-called mini-, micro, nano-, pico- and femto-, as well as CubeSat, spacecraft. Therefore, for the sake of convenience, the term "small spacecraft" is used throughout this document as a generic term.

ISO 19683:2017 includes CubeSat, as long as it is developed with the untraditional processes.

标准预览图