BS ISO 11892-2012 Space systems Subsystems units to spacecraft interface control document《空间系统 子系统 单元宇宙飞船接口控制文件》.pdf
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1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationSpace systems Subsystems/units to spacecraft interface control documentBS ISO 11892:2012National forewordThis British Standard is the UK implementation of ISO 11892:2012.The UK p
2、articipation in its preparation was entrusted by Technical CommitteeACE/68, Space systems and operations, to Panel ACE/68/-/2, Space systems and operations - Interfaces, integration and test.A list of organizations represented on this committee can be obtained on request to its secretary.This public
3、ation does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. The British Standards Institution 2012Published by BSI Standards Limited 2012 ISBN 978 0 580 74032 9 ICS 49.140Compliance with a British Standard cannot confer immunity fr
4、om legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy Committee on 30 April 2012.Amendments issued since publicationAmd. No. Date Text affectedBRITISH STANDARDBS ISO 11892:2012 ISO 2012Space systems Subsystems/units to spacecraft interface
5、control documentSystmes spatiaux Document de contrle des interfaces entre les sous-systmes/units et le vhicule spatialINTERNATIONAL STANDARDISO11892First edition2012-03-01Reference numberISO 11892:2012(E)BS ISO 11892:2012ISO 11892:2012(E)ii ISO 2012 All rights reservedCOPYRIGHT PROTECTED DOCUMENT IS
6、O 2012All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without permission in writing from either ISO at the address below or ISOs member body in the
7、country of the requester.ISO copyright officeCase postale 56 CH-1211 Geneva 20Tel. + 41 22 749 01 11Fax + 41 22 749 09 47E-mail copyrightiso.orgWeb www.iso.orgPublished in SwitzerlandBS ISO 11892:2012ISO 11892:2012(E) ISO 2012 All rights reserved iiiContents PageForeword iv1 Scope 12 Normative refer
8、ences . 13 Terms, definitions and abbreviated terms 13.1 Terms and definitions . 13.2 Abbreviated terms . 24 Subsystem to spacecraft ICD . 24.1 General . 24.2 Cover sheet . 44.3 Applicability 44.4 List of units . 44.5 Subsystem block diagram 54.6 Subsystem grounding diagram . 54.7 Subsystem operatio
9、nal mode definition (if applicable) 54.8 Unit ICD (if applicable) . 54.9 Co-axial cable or waveguide ICD (if applicable) . 54.10 Wire harness ICD (if applicable) 55 Unit ICD in detail 55.1 General . 55.2 Cover sheet . 65.3 Interface data sheet (IDS) 75.4 Pin assignment table 135.5 Telemetry command
10、list 135.6 Input/output circuits .135.7 Grounding diagram .145.8 Outline drawing 145.9 Three-dimensional CAD model (if applicable) .145.10 Non-removal test items (if applicable) .145.11 Related technical documents (if applicable) 146 Verification 156.1 General .156.2 Verification method .15Bibliogra
11、phy .16BS ISO 11892:2012ISO 11892:2012(E)ForewordISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical committees. Each member bo
12、dy interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrot
13、echnical Commission (IEC) on all matters of electrotechnical standardization.International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2.The main task of technical committees is to prepare International Standards. Draft International Standards adopted by
14、the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote.Attention is drawn to the possibility that some of the elements of this document may be the subject of patent right
15、s. ISO shall not be held responsible for identifying any or all such patent rights.ISO 11892 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 14, Space systems and operations.iv ISO 2012 All rights reservedBS ISO 11892:2012INTERNATIONAL STANDARD ISO 11892:2
16、012(E)Space systems Subsystems/units to spacecraft interface control document1 ScopeThis International Standard provides space system manufacturing organizations with the minimum interface related items and generic format for creating the interface control document (ICD) which subsystems or units su
17、ppliers prepare for spacecraft systems (SC) integrators.In this International Standard, ICD is not defined to contain descriptions regarding various properties of subsystems or units or tasks to be done by suppliers, i.e. performance, functions, endurance to launch mechanical environment, or quality
18、 assurance provisions. Such descriptions are presumed to be defined in other contractual documents such as technical specifications.2 Normative referencesThe following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. F
19、or undated references, the latest edition of the referenced document (including any amendment) applies.ISO 15864:2004, Space systems General test methods for space craft, subsystems and units3 Terms, definitions and abbreviated terms3.1 Terms and definitions3.1.1subsystemassembly or group of electri
20、cal, thermal and/or mechanical units which is dedicated to specific functions of a spacecraft system (SC)3.1.2unitindependently handled device at the lowest level of hardware assembly that works with specified complex electrical, thermal and/or mechanical functionsNOTE Several units build up a subsy
21、stem. A single unit may occasionally comprise a subsystem by itself.3.1.3subsystems/units to spacecraft interface control documentset of documents that defines and controls the electrical, thermal, and mechanical interface requirements between a subsystem and the spacecraft system (SC)NOTE Figure 1
22、illustrates the hierarchy of a space system and the ranges where various interface control documents are applicable. ISO 2012 All rights reserved 1BS ISO 11892:2012ISO 11892:2012(E)Spacecraft to launch vehicle ICD Subsystems or units to spacecraft ICD Unit ICDSpace system Spacecraft system Subsystem
23、-ASubsystem-C Subsystem-B Wire harness Co-axial cable/waveguide Unit-A Unit-B Unit-C Co-axial cable/waveguide Wire harness Launch vehicle Hierarchy of a space system and related interface control document (ICD)3.2 Abbreviated termsCAD computer aided designICD interface control documentIDS interface
24、data sheetMOI moment of inertiaRF radio frequency4 Subsystem to spacecraft ICD4.1 GeneralA subsystem ICD is a package constructed of sub-documents as shown in Table 1. It shall contain configuration control information, subsystem definition diagrams, and if applicable, co-axial cable or waveguide or
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