欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    SAE EIA-649-2-2016 Configuration Management Requirements for NASA Enterprises.pdf

    • 资源ID:1026026       资源大小:336.64KB        全文页数:48页
    • 资源格式: PDF        下载积分:10000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要10000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    SAE EIA-649-2-2016 Configuration Management Requirements for NASA Enterprises.pdf

    1、 _ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSXEOLVKH GE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJL neering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole re

    2、sponsibility RIWKHXVHU SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2016 SAE International All rights reserved. No part of this publication may be reprod

    3、uced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724

    4、-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/EIA649-2 TECHNICAL REPORT EIA-649-2 Issued 2016-04 Configuration Management Requirements for NASA Enterpr

    5、ises RATIONALE This companion standard to “SAE/EIA-649B Configuration Management Standard,“ is needed to provide a resource that standardizes Configuration Management (CM) requirements specific to National Aeronautics and Space Administration (NASA) agreements and design activities. This Standard pr

    6、ovides a template of CM requirements and user guidance for tailoring the requirements for each unique use case. This standard has been revised to incorporate content changes proposed by the G33 Committee that were not included in the original release. FOREWORD SAE International publishes this compan

    7、ion standard to the NASA-endorsed SAE/EIA-649B for NASA to provide uniform CM requirements for NASA enterprise agreements and activities. The Office of the Chief Engineer-NASA Headquarters, the NASA Field Centers, including Component Facilities, and the SAE governing CM Council, approve this Standar

    8、d for use. This document is used as a stand-alone reference, invoked by an agreement where the customer intends to be consistent with the NASA-endorsed ANSI/EIA-649 principles, and may be used for all NASA enterprises in all phases of the program/project/activity life cycle. We also acknowledge the

    9、NASA CM Community of Practice, the NASA CM Standards Project Team, and the SAE G33 Committee for their support in developing this companion standard. SAE INTERNATIONAL EIA-649-2 Page 2 of 48 INTRODUCTION This Standard provides a consistent and systematic set of requirements that are used for the man

    10、agement of Configuration Items (CIs) delivered to, or produced by, the Agency that does the following: a. Identifies the configuration of a product at various points throughout its life cycle; b. Systematically controls changes to the configuration of the product; c. Maintains the integrity and trac

    11、eability of the configuration of the item throughout its life; and d. Preserves the information for the product configuration. The requirements support the planning and implementation of a Configuration Management (CM) system as described by the functions and principles of SAE/EIA-649B. The requirem

    12、ents are grouped using the five functions: (1) CM Planning; (2) Configuration Identification (including interface management); (3) Change Management (Configuration Control); (4) Configuration Status Accounting (CSA) (including configuration traceability); and (5) Configuration Verification and Audit

    13、s. Requirements are numbered and indicated by the word “shall.“ Explanatory or guidance text is indicated in italics beginning in Section 4. NOTE: For simplicity, when this document uses the term Configuration Item (CI), the requirement or guidance presumes the inclusion of all computer software con

    14、figuration items (CSCIs), unless otherwise specified. All CSCIs which are selected by the Customer are subject to the same criteria as are hardware elements designated as CIs. Applicable general NASA CM policy that contains parent requirements and definitions are captured in Table 1. Table 1 - NASA

    15、configuration management policy Standard Number Standard Title NPD 7120.4D NASA Engineering and Program/Project Management Policy NPR 7120.5E NASA Space Flight Program and Project Management Requirements NPR 7120.8 NASA Research and Technology Program and Project Management Requirements NPR 7120.9 N

    16、ASA Product Data and Life-Cycle Management (PDLM) for Flight Programs and Projects NPR 7123.1B NASA Systems Engineering Processes and Requirements NPR 7150.2B NASA Software Engineering Requirements SAE INTERNATIONAL EIA-649-2 Page 3 of 48 TABLE OF CONTENTS 1. SCOPE 4 1.1 Responsibility of Customer a

    17、nd Suppliers. 4 1.1.1 Responsibility of Customer 4 1.1.2 Responsibility of Supplier 4 1.2 Requirements Approach . 4 1.2.1 Tailoring . 4 1.2.2 Requirements Verb Usage 5 2. REFERENCES 5 2.1 Applicable Documents 5 2.1.1 SAE Publications . 5 2.1.2 Other Documents 5 2.2 Related Publications 6 2.3 Definit

    18、ions 6 2.4 Acronyms/Abbreviations 11 3. GENERAL CONFIGURATION MANAGEMENT REQUIREMENTS . 12 3.1 Configuration Management Application 12 3.1.1 Supplier Configuration Management Planning 14 3.2 Configuration Identification 15 3.2.1 General Requirements 16 3.2.2 Configuration Item Selection . 16 3.2.3 C

    19、onfiguration Baselines and their Configuration Information 16 3.2.4 Configuration Identifiers 19 3.3 Configuration Change Management . 22 3.3.1 Configuration Control Boards 23 3.3.2 Preparation of Change and Variance Request . 24 3.3.3 Major and Minor Changes . 26 3.3.4 Change Request Supporting Dat

    20、a 27 3.3.5 Software Change Control 27 3.3.6 As-Built Change Management 27 3.3.7 As-Deployed Change Management 28 3.3.8 Modification Kit and Instructions 29 3.4 Configuration Status Accounting . 29 3.4.1 CSA Requirements . 29 3.5 Configuration Verification and Audits 31 3.5.1 In-Process Configuration

    21、 Management Audits 31 3.5.2 Common Audit Responsibilities 32 3.5.3 Functional Configuration Audit 35 3.5.4 Physical Configuration Audit . 38 3.5.5 Post-Audit Action . 43 3.5.6 Configuration Audit Summary . 43 3.6 Enabling General Requirements . 43 3.6.1 Engineering Release . 43 3.6.2 Interface Manag

    22、ement 45 3.6.3 Performance Measurement 47 4. NOTES 47 4.1 CM Related Data Management . 47 4.2 Revision Indicator 48 SAE INTERNATIONAL EIA-649-2 Page 4 of 48 1. SCOPE This Standard applies to all products produced by NASA Headquarters and NASA Centers, including Component Facilities and Technical and

    23、 Service Support Centers. This Standard may also apply to the Jet Propulsion Laboratory and suppliers/service providers to the extent specified in their agreements with NASA. This Standard may be cited in the CM requirements of NASA Headquarters, NASA Centers, Programs, Projects, and Supplier agreem

    24、ents. NOTE: 7KHXVHRIWKHWHUPD greement V LQFOXGHVFRQWUDFWVDQGOHVVIRUPDOLWHPVVXFKDVWDVNDJUHHPHQWV This Standard is also applicable to NASA investment areas covered under NPR 7120.5, NPR 7120.7, and NPR 7120.8. This Standard may be further applied to other NASA investments at the discretion of NASA man

    25、agement. This Standard applies throughout all phases of the program and project life cycle. NOTE: While this Standard is released by SAE International, it is an endorsed standard for use by NASA. 1.1 Responsibility of Customer and Suppliers 1.1.1 Responsibility of Customer The Customer establishes a

    26、nd controls the products functional and performance requirements, and has oversight and agreement compliance responsibility during product development, deployment, operation, upgrade/ modification, maintenance, and disposal. The Customer defines agreement CM terminology and unique CM application for

    27、 agreement(s) through tailoring of this Standard. The Customer may cite the untailored requirements of this companion Standard, or create a set of tailored requirements either of which may be included as part of internal agreements for NASA programs and projects. 1.1.2 Responsibility of Supplier The

    28、 Supplier is responsible for complying with the requirements contained in this Standard as tailored by the Customer. In addition, the Supplier is responsible for ensuring that their sub-tier suppliers also comply with the tailored requirements, when needed to assure that the overall CM system is eff

    29、icient and interoperable. 1.2 Requirements Approach 1.2.1 Tailoring The requirements in this Standard are included in agreements only to the extent specified for each unique agreement. The Customer is responsible for tailoring the requirements from this Standard to develop and invoke a unique set of

    30、 CM requirements for each agreement or internal development activity. Factors that influence tailoring include the programs or SURMHFWVOLIHFFOHSKDVHDJUHHPHQWWSHDQGVWUXFWXUHFRPSOHLWVFRSHLQWHQGHGXVHU LVN-tolerance, and mission criticality for the identified CIs. A specific tailoring guideline matrix i

    31、s provided at the following location on the NASA Engineering Network - SAE 649-2 Tailoring Matrix. This matrix, which is structured in accordance with NASA project classifications, is provided as an aid to the Customer in tailoring these requirements. The parent Standard to this companion Standard,

    32、ANSI/EIA-649, contains principles listed in this document that are copyright-protected by SAE. The principles contained in this Standard are intended to be for reference only. Except as permitted under the applicable laws of the users country, neither the SAE/ANSI/EIA-649B principles nor any extract

    33、 may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, whether electronic, photocopying, recording, or otherwise, without prior written permission being secured; they are intended to be for reference only. SAE INTERNATIONAL EIA-649-2 Page 5 of 48 1.2.2 Requirem

    34、ents Verb Usage a. 6KDOOLVXVHGWRLQGLFDWHDUHTXLUHPHQWWKDWLVELQGLQJZKLFKPXVWEHLPSOHP HQWHGDQGLWVLPSOHPHQWDWLRQYHULILHGLQthe approach, planning, and implementation. b. 6KRXOGLVXVHGWRLQGLFDWHEHVWSUDFWLFHRUDJRDOWKDWLVGHVLUDEOHEXWQRWPDQGDWRU c. 0DLVXVHGWRLQGLFDWHSHUPLVVLRQ d. :LOOLVXVHGWRLQGLFDWHDVWDWHPHQ

    35、WRIIDFWRUGHFODUDWLRQRISXUSRVHRQW he part of the Customer that is reflective of decisions or realities that exist and are to be taken as a given and not open to debate or discussion. e. ,VRU$UHDUHXVHGWRLQGLFDWHGHVFULSWLYHFRQWHQW 2. REFERENCES 2.1 Applicable Documents The following publications form a

    36、 part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references cited herein,

    37、the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insi

    38、de USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. SAE/EIA-649B Configuration Management Standard (referred to in this Standard as EIA-649) 2.1.2 Other Documents ANSI/EIA-836 Configuration Management - Data Exchange and Interoperability ASME Y14.24 Types and Applications of Engineerin

    39、g Drawings ASME Y14.100 Engineering Drawing and Related Information Practices DD Form 250 (DOD) Material Inspection and Receiving Report DD Form 1149 Requisition and Invoice/Shipping Document (for Government to Government transfer) DRD-STD-AD Functional Configuration/Physical Configuration Audit DRD

    40、-STD-CR Change Request DRD-STD-CMP Configuration Management Plan DRD-STD-CMPA Configuration Management Process Audit DRD-STD-CSA Configuration Status Accounting DRD-STD-EDAL Engineering Drawing and Associated List DRD-STD-MINC Modification Kit and Instructions SAE INTERNATIONAL EIA-649-2 Page 6 of 4

    41、8 DRD-STD-SDT Specification and Drawing Tree DRD-STD-VDD Version Description Document DRD-STD-VR Variance Request MIL-STD-130 Identification Marking of U.S. Military Property MIL-STD-31000 Technical Data Packages NAS 3500 Technical Data Package: Composition, Communication, and Application NID 1600.5

    42、5 Sensitive But Unclassified (SBU) Controlled Information NPR 1441.1 Records Retention Schedules NPR 7120.5 Spaceflight Program and Project Management Requirements NPR 7120.7 Information Technology and Institutional Infrastructure Program and Project Requirements NPR 7120.8 Research and Technology P

    43、rogram and Project Management Requirements NPR 7150.2 NASA Software Engineering Requirements NPR 8735.1 Exchanging Parts, Materials, Software, and Safety Problem Data Utilizing the Government-Industry Data Exchange Program (GIDEP) 2.2 Related Publications None. 2.3 Definitions Because this Standard

    44、has application across many diverse industries and governmental activities in which terminology differs, common terminology is used as much as possible. The terms apply to whatever is common to any particular user environment through the concepts inherent in their definitions. This section aids in u

    45、nderstanding equivalency of terms by defining the terms used within this Standard and addressing aliases (commonly used terms that convey the same or similar meaning) and other closely related terms where known aliases exist. For purposes of this Standard, the definitions contained in the parent sta

    46、ndard SAE/EIA-649B, as well as the additional terms below apply. When planning and documenting a CM system, a Customer may substitute aliases or any other terms familiar to their environment for the terminology used within this Standard. There is also no intent to rigidly adhere to the terminology within this Standard if, in specific instances, use of an alias provides clarity. However, the application of terminology to the requirements contained herein should be carefully cons


    注意事项

    本文(SAE EIA-649-2-2016 Configuration Management Requirements for NASA Enterprises.pdf)为本站会员(twoload295)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1 

    收起
    展开