ISO 27875 AMD 1-2016 Space systems - Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages Amendment 1《航天系统 无人飞船和运载火箭轨道级用回港风险管理 修改件.pdf

《ISO 27875 AMD 1-2016 Space systems - Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages Amendment 1《航天系统 无人飞船和运载火箭轨道级用回港风险管理 修改件.pdf》由会员分享，可在线阅读，更多相关《ISO 27875 AMD 1-2016 Space systems - Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages Amendment 1《航天系统 无人飞船和运载火箭轨道级用回港风险管理 修改件.pdf（8页珍藏版）》请在麦多课文档分享上搜索。

1、 ISO 2016 Space systems Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages AMENDMENT 1 Systmes spatiaux Gestion du risque de la rentre pour les tapes orbitales des vhicules spatiaux non habits et des lanceurs spatiaux AMENDEMENT 1 INTERNATIONAL STANDARD ISO 27875 Firs

2、t edition 2010-03-01 Reference number ISO 27875:2010/Amd.1:2016(E) AMENDMENT 1 2016-03-15 ISO 27875:2010/Amd.1:2016(E)ii ISO 2016 All rights reserved COPYRIGHT PROTECTED DOCUMENT ISO 2016, Published in Switzerland All rights reserved. Unless otherwise specified, no part of this publication may be re

3、produced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting on the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below or ISOs member body in the country of the reques

4、ter. ISO copyright office Ch. de Blandonnet 8 CP 401 CH-1214 Vernier, Geneva, Switzerland Tel. +41 22 749 01 11 Fax +41 22 749 09 47 copyrightiso.org www.iso.org ISO 27875:2010/Amd.1:2016(E) Foreword ISO (the International Organization for Standardization) is a worldwide federation of national stand

5、ards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International orga

6、nizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. The procedures used to develop this document and those intended for its

7、 further maintenance are described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed for the different types of ISO documents should be noted. This document was drafted in accordance with the editorial rules of the ISO/IEC Directives, Part 2 (see www.iso.org/dir

8、ectives). Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of any patent rights identified during the development of the document will be in t

9、he Introduction and/or on the ISO list of patent declarations received (see www.iso.org/patents). Any trade name used in this document is information given for the convenience of users and does not constitute an endorsement. For an explanation on the meaning of ISO specific terms and expressions rel

10、ated to conformity assessment, as well as information about ISOs adherence to the WTO principles in the Technical Barriers to Trade (TBT) see the following URL: Foreword - Supplementary information The committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcommittee SC

11、 14, Space systems and operations. ISO 2016 All rights reserved iii Space systems Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages AMENDMENT 1 Page 1, Normative references Add the following reference: ISO 10795, Space systems Programme management and quality Vocabul

12、ary Page 1, Terms and definitions Replace the introductory text for Terms and definitions with the following: For the purposes of this document, the terms and definitions given in ISO 10795 and the following apply. Page 1, Terms and definitions Replace entry 3.2 with the following: 3.2 launch vehicl

13、e orbital stage stage of a launch vehicle that is designed to achieve orbit Page 2, Terms and definitions Replace entry 3.3 with the following: 3.3 re-entry return of a spacecraft or other man-made space object into the Earths atmosphere ISO 27875:2010/Amd.1:2016(E) ISO 2016 All rights reserved 1 IS

14、O 27875:2010/Amd.1:2016(E) Page 5, Figure 1 Replace Figure 1 with the following: START Survivability analysis Completely demised or something survival? Complete Demise Risk to human : threshold On the Earth, environment : threshold Disposal by natural decay or reduction of orbital lifetime (uncontro

15、lled re-entry) Some Survivalthreshold threshold Impossible Possible START Survivability analysis Complete demise Completely demised or something survived? Some survival Risk to human : thresholdthreshold threshold Page 6, Clause 7 Delete Clause 7. Page 10, Clause A.6 Delete Clause A.6.2 ISO 2016 All rights reserved ISO 27875:2010/Amd.1:2016(E) ISO 2016 All rights reserved IC S 49.140 Price based on 2 pages