BS ISO 19683:2017规定了设计鉴定和/或验收的试验方法和试验要求 指小型航天器或装置。它提供了最低测试要求和测试方法，以鉴定 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。本文件强调了在卫星发射后实现婴儿死亡率的可靠性 在轨运行，同时保持低成本和快速交付。本文件适用于开发方法与使用方法不同的卫星 对于风险承受空间很小的传统卫星，如图1所示。这个范围 该文件涵盖了不同类别的小型航天器，即所谓的微型航天器- ，微米，纳米，皮卡和 femto-以及CubeSat航天器。因此，为了方便起见，“小”一词 本文件通篇使用“航天器”作为通用术语。交叉引用:ISO 17566:2011 Ed 1ISO 14302:2002 Ed 1ISO 15864:2004 Ed 1ISO 11221:2011 Ed 1ECSS-E-ST-40CDOE-NE-STD.1004-92MIL-STD.461NASA-STD.7003ASMC-S-016NASA-STD.7001AISO 17770:2017ISO 26869:2012ISO 24113:2011 Ed 2ISO 14620-1:2002购买本文件时可提供的所有现行修订版。

BS 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.This document places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low cost and fast delivery.This document 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-, picoand 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.Cross References:ISO 17566:2011 Ed 1ISO 14302:2002 Ed 1ISO 15864:2004 Ed 1ISO 11221:2011 Ed 1ECSS-E-ST-40CDOE-NE-STD.1004-92MIL-STD.461NASA-STD.7003ASMC-S-016NASA-STD.7001AISO 17770:2017ISO 26869:2012ISO 24113:2011 Ed 2ISO 14620-1:2002All current amendments available at time of purchase are included with the purchase of this document.