BS ISO 16126-2014 Space systems Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal《空间系统 为确保成功后.pdf
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1、BSI Standards PublicationBS ISO 16126:2014Space systems Assessmentof survivability of unmannedspacecraft against space debrisand meteoroid impacts toensure successful post-missiondisposalBS ISO 16126:2014 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of ISO 16126:20
2、14.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/68/-/1, Space systems and operations - Design,Engineering and Production.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include al
3、l the necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2014. Published by BSI StandardsLimited 2014ISBN 978 0 580 69946 7ICS 49.140Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standa
4、rd was published under the authority of theStandards Policy and Strategy Committee on 30 April 2014.Amendments issued since publicationDate Text affectedBS ISO 16126:2014 ISO 2014Space systems Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure suc
5、cessful post-mission disposalSystmes spatiaux valuation de la capacit de survie des vhicules spatiaux non habits face aux dbris spatiaux et aux impacts de mtorodes pour garantir une limination efficace daprs-missionINTERNATIONAL STANDARDISO16126First edition2014-04-01Reference numberISO 16126:2014(E
6、)BS ISO 16126:2014ISO 16126:2014(E)ii ISO 2014 All rights reservedCOPYRIGHT PROTECTED DOCUMENT ISO 2014All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, o
7、r 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 requester.ISO copyright officeCase postale 56 CH-1211 Geneva 20Tel. + 41 22 749 01 11Fax + 41 22 749 09 47E-mail copy
8、rightiso.orgWeb www.iso.orgPublished in SwitzerlandBS ISO 16126:2014ISO 16126:2014(E) ISO 2014 All rights reserved iiiContents PageForeword iv1 Scope . 12 Normative references 13 Terms and definitions . 14 Abbreviated terms 35 Impact survivability assessment requirements 36 Impact survivability asse
9、ssment procedure . 36.1 General . 36.2 Definition of survivability requirement 36.3 Impact risk analysis 37 Procedure for performing a simple impact risk analysis 47.1 General . 47.2 Spacecraft operating parameters and architecture design . 57.3 Identification of critical components and surfaces . 5
10、7.4 Ballistic limits . 57.5 Failure probability analysis 57.6 Completion of analysis . 68 Procedure for performing a detailed impact risk analysis 68.1 General . 68.2 Spacecraft operating parameters and architecture design . 68.3 Identification of critical components. 68.4 Ballistic limits . 78.5 Fa
11、ilure probability analysis 88.6 Iteration of analysis. 8Annex A (informative) Supplementary information on the simple impact risk analysis procedure 10Annex B (informative) Ballistic limit equations 12Annex C (informative) Background information on hypervelocity impact testing and modelling 14Annex
12、D (informative) Method to calculate impact-induced Probability of No Failure .16Annex E (informative) Options for improving impact survivability .17Bibliography .19BS ISO 16126:2014ISO 16126:2014(E)ForewordISO (the International Organization for Standardization) is a worldwide federation of national
13、 standards 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. Internationa
14、l organizations, 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 fo
15、r its 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.or
16、g/directives). 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
17、 in the 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
18、 related 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 informationThe committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcommittee
19、 SC 14, Space systems and operations.iv ISO 2014 All rights reservedBS ISO 16126:2014INTERNATIONAL STANDARD ISO 16126:2014(E)Space systems Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal1 ScopeThis International
20、 Standard defines requirements and a procedure for assessing the survivability of an unmanned spacecraft against space debris and meteoroid impacts to ensure the survival of critical components required to perform post-mission disposal. This International Standard also describes two impact risk anal
21、ysis procedures that can be used to satisfy the requirements. The procedures are consistent with those defined in References 1 and 2.This International Standard is part of a set of International Standards that collectively aim to reduce the growth of space debris by ensuring that spacecraft are desi
22、gned, operated, and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime. All of the primary debris mitigation requirements are contained in a top-level International Standard.3The remaining International Standards, of which this is one, provide methods
23、 and processes to enable compliance with the primary requirements.2 Normative referencesThe following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, t
24、he latest edition of the referenced document (including any amendments) applies.ISO 10795:2011, Space systems Programme management and quality Vocabulary3 Terms and definitionsFor the purposes of this document, the terms and definitions given in ISO 10795:2011 and the following apply.3.1at-risk area
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