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现行 ISO 14621-2:2019
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Space systems — Electrical, electronic and electromechanical (EEE) parts — Part 2: Control programme requirements 航天系统.电气 电子和机电(EEE)部件.第2部分:控制程序要求
发布日期: 2019-05-23
本文件确立了制定和记录电气、电子和机电(EEE)部件控制程序的技术指南,以确保飞行硬件中使用的部件是可接受的,并具有足够的功能、辐射和可靠性特性,以满足系统要求。EEE零件系列包括光电零件。 本文件确定了一套处理空间系统工程活动的管理准则,并定义了该主题的最低现有流程。 根据项目绩效标准、风险承受能力、预算、任务期限、环境、进度和其他考虑因素,这些指导方针可根据每个项目的需求进行调整。本文件适用于所有提供飞行硬件的客户和供应商,并适合在建议书说明中参考。
This document establishes technical guidelines for developing and documenting an electrical, electronic and electromechanical (EEE) parts control program, in order to assure that the parts used in the flight hardware are acceptable and possess adequate functional, radiation and reliability characteristics to meet the system requirements. The family of EEE parts includes electro-optical parts. This document identifies a set of management guidelines for dealing with space systems engineering activities and defines the minimum existing processes on the subject. These guidelines are tailorable to the needs of each individual programme based on the project performance criteria, risk tolerance, budget, mission duration, environment, schedule and other considerations. This document is applicable to all customers and suppliers furnishing flight hardware and is suitable for reference in proposal instructions.
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归口单位: ISO/TC 20/SC 14
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