EN 16604-10-2014 en Space sustainability - Adoption Notice of ISO 24113 Space systems - Space debris mitigation requirements《空间持续性 ISO 24113的采用注意 空间系统 空间残骸减轻的要求》.pdf

《EN 16604-10-2014 en Space sustainability - Adoption Notice of ISO 24113 Space systems - Space debris mitigation requirements《空间持续性 ISO 24113的采用注意 空间系统 空间残骸减轻的要求》.pdf》由会员分享，可在线阅读，更多相关《EN 16604-10-2014 en Space sustainability - Adoption Notice of ISO 24113 Space systems - Space debris mitigation requirements《空间持续性 ISO 24113的采用注意 空间系统 空间残骸减轻的要求》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、BSI Standards PublicationBS EN 16604-10:2014Space sustainability Adoption Notice of ISO 24113:Space systems Space debrismitigation requirementsBS EN 16604-10:2014 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 16604-10:2014.The UK participation in its preparati

2、on was entrusted to TechnicalCommittee ACE/68, Space systems and operations.A list of organizations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct

3、 application. The British Standards Institution 2014.Published by BSI Standards Limited 2014ISBN 978 0 580 84103 3 ICS 49.140 Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy

4、Committee on 30 September 2014.Amendments/corrigenda issued since publicationDate T e x t a f f e c t e dEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16604-10 September 2014 ICS 49.140 English version Space sustainability - Adoption Notice of ISO 24113: Space systems - Space debris mitigatio

5、n requirements Dveloppement durable de lespace - Notice dadoption de la norme ISO 24113: Systmes spatiaux - Exigences relatives la rduction des dbris spatiaux Nachhaltigkeit im Weltraum - bernahmebemerkung zu ISO 24113: Space systems - Space debris mitigation requirements This European Standard was

6、approved by CEN on 1 March 2014. CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning

7、 such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN and CENELEC member. This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN and

8、 CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Den

9、mark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. CEN-CENELEC Manag

10、ement Centre: Avenue Marnix 17, B-1000 Brussels 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16604-10:2014 EBS EN 16604-10:2014Table of contents Foreword 3 1 Scope . 4 2 Context information 5

11、 3 Application requirements 6 Tables Table 3-1: Applicability table for ISO 24113 6 EN 16604-10:2014 (E)BS EN 16604-10:2014Foreword This document (EN 16604-10:2014) has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16604-10:2014

12、) originates from ECSS-U-AS-10C. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by March 2015, and conflicting national standards shall be withdrawn at the latest by March 2015. Attention is drawn t

13、o the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. This document has been prepared under a mandate given to CEN by the European Commission and the European F

14、ree Trade Association. This document has been developed to cover specifically space systems and has therefore precedence over any EN covering the same scope but with a wider domain of applicability (e.g. : aerospace). According to the CEN-CENELEC Internal Regulations, the national standards organiza

15、tions of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Mal

16、ta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. EN 16604-10:2014 (E)BS EN 16604-10:20141 Scope This document identifies the clauses and requirements modified with respect to the standard ISO 24113, Space systems Space

17、 debris mitigation requirements, Second edition 2011-05-15 for application in ECSS. EN 16604-10:2014 (E)BS EN 16604-10:20142 Context information The standard ISO 24113, Space systems Space debris mitigation requirements has been developed by ISO TC20/SC14. The key space debris mitigation requirement

18、s have been thoroughly discussed at international level, agreed by the ISO members and published as standard ISO 24113. Aiming at the development of world wide implementation standards dealing with space debris mitigation, ECSS has proactively contributed to the preparation of ISO 24113. ECSS decide

19、d to adopt and apply ISO 24133 with a minimum set of modifications, identified in the present document, to account for the reference and applicable space debris mitigation documents existing in Europe and of the needs of the ECSS members. EN 16604-10:2014 (E)BS EN 16604-10:2014Clause orrequirement n

20、umber Applicability Applicable text (the new/added text is underlined) Comments Text as in the original document (deleted text with strikethrough) 6.1.1.3 Newrequirement If space debris are released into Earth orbitduring normal launch operations, then thenumber of space debris released, other thant

21、hose covered by 6.1.2, shall not exceed: a. One, for the launch of a single spacecraft. b. Two, for the launch of multiple spacecraft. New requirement added - 6.1.2.2 Modified (whole text ofthe requirement) Solid rocket motors shall be designed andoperated to avoid releasing solid combustionproducts

22、 larger than 1 mm into the GEOprotected region. ISO requirement modified toinclude the maximum size ofsolid combustion products. Solid rocket motors shall be designed andoperated so as to avoid releasing solidcombustion products into the GEO protectedregion. EN 16604-10:2014 (E)BS EN 16604-10:2014BS

23、 EN 16604-10:20143Application requirements a. ISO 24113, Space systems - Space debris mitigation requirements, Second edition 2011-05-15 shall apply with the modifications listed inTable 3-1. Table 3-1: Applicability table for ISO 24113 Clause orrequirement number Applicability Applicable text (the

24、new/added text is underlined) Comments Text as in the original document (deleted text with strikethrough) 1 Scope (1stparagraph)Modified This International Standard defines theprimary space debris mitigation re-quirements applicable to all elements ofsystems launched into or passing throughnear-Eart

25、h space, including launch vehicleorbital stages, operating spacecraft, and anyobjects released as part of normal operations or disposal actions. Word “unmanned” deleted fromthe Scope of the ISO standard. This International Standard defines theprimary space debris mitigationrequirements applicable to

26、 all elements ofunmanned systems launched into 3.15 re-entry Modified (NOTEdeleted) process in which atmospheric drag cascadesdeceleration of a spacecraft or launch vehicleorbital stage (or any part thereof), leading toits destruction or return to Earth NOTE deleted process in which atmospheric drag

27、 cascadesdeceleration of a spacecraft or launch vehicleorbital stage (or any part thereof), leading toits destruction or return to Earth NOTE For operational purposes, this iswhen the period of the mean orbit is 89 minutes or less.“ EN 16604-10:2014 (E)BS EN 16604-10:2014This page deliberately left

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