BS EN 16602-70-04-2014 Space product assurance Thermal testing for the evaluation of space materials processes mechanical parts and assemblies《航天产品保证 用于评估空间材料 过程 机械零件和装配件的热工测试》.pdf
《BS EN 16602-70-04-2014 Space product assurance Thermal testing for the evaluation of space materials processes mechanical parts and assemblies《航天产品保证 用于评估空间材料 过程 机械零件和装配件的热工测试》.pdf》由会员分享,可在线阅读,更多相关《BS EN 16602-70-04-2014 Space product assurance Thermal testing for the evaluation of space materials processes mechanical parts and assemblies《航天产品保证 用于评估空间材料 过程 机械零件和装配件的热工测试》.pdf(28页珍藏版)》请在麦多课文档分享上搜索。
1、BSI Standards PublicationBS EN 16602-70-04:2014Space product assurance Thermal testing for theevaluation of space materials,processes, mechanical partsand assembliesBS EN 16602-70-04:2014 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN16602-70-04:2014. It supers
2、edes BS EN 14098:2001 which iswithdrawn.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/68, Space systems and operations.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all t
3、he necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2014. Published by BSI StandardsLimited 2014ISBN 978 0 580 84423 2ICS 49.140Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard
4、was published under the authority of theStandards Policy and Strategy Committee on 31 October 2014.Amendments issued since publicationDate Text affectedBS EN 16602-70-04:2014EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16602-70-04 October 2014 ICS 49.140 Supersedes EN 14098:2001 English vers
5、ion Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies Assurance produit des projets spatiaux - Essais thermiques pour lvaluation des matriaux, des processus, des composants et assemblages mcaniques dun projet spatial Raumfahrt
6、produktsicherung - Temperaturtest zur Untersuchung von Werkstoffen, Prozessen, mechanischen Teilen und Zusammenbauten der Raumfahrttechnik This European Standard was approved by CEN on 20 March 2014. CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulat
7、e the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN and CENELEC member. This E
8、uropean 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 CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions.
9、 CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lit
10、huania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved wor
11、ldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16602-70-04:2014 EBS EN 16602-70-04:2014EN 16602-70-04:2014 (E) 2 Table of contents Foreword 4 Introduction 5 1 Scope . 6 2 Normative references . 7 3 Terms, definitions and abbreviated terms 8 3.1 Terms from other standards 8 3.2
12、Terms specific to the present standard . 8 3.3 Abbreviated terms. 8 4 Principles 9 5 Requirements 11 5.1 Specifying test 11 5.1.1 General provision 11 5.1.2 Specifying the test means . 11 5.1.3 Specifying the thermal cycling test procedures 12 5.2 Preparing and performing Test . 13 5.2.1 General . 1
13、3 5.2.2 Preparing the item to be tested . 13 5.2.3 Preparing the facilities and equipment. 14 5.2.4 Running the thermal cycling test procedures . 14 5.3 Recording and reporting the test results . 15 5.3.1 Test records 15 5.3.2 Test report 16 5.3.3 Acceptance criteria and nonconformance . 16 Annex A
14、(normative) Request for thermal cycling test - DRD . 17 Annex B (normative) Thermal cycling test specifications and procedures (Work Proposal) - DRD 18 Annex C (normative) Thermal cycling test report - DRD 19 BS EN 16602-70-04:2014EN 16602-70-04:2014 (E) 3 Annex D (informative) Thermal cycling test
15、procedures . 20 Annex E (informative) Thermal cycling test equipment . 23 Bibliography . 24 Figures Figure 4-1: Thermal cycling test process overview . 9 Figure D-1 : Test procedure flow diagram 22 BS EN 16602-70-04:2014EN 16602-70-04:2014 (E) 4 Foreword This document (EN 16602-70-04:2014) has been
16、prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-70-04:2014) originates from ECSS-Q-ST-70-04C. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement,
17、at the latest by April 2015, and conflicting national standards shall be withdrawn at the latest by April 2015. Attention is drawn to 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 o
18、r all such patent rights. This document supersedes EN 14098:2001. This document has been prepared under a mandate given to CEN by the European Commission and the European Free Trade Association. This document has been developed to cover specifically space systems and has therefore precedence over an
19、y 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 organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Cze
20、ch Republic, Denmark, 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 the United Kingdo
21、m. BS EN 16602-70-04:2014EN 16602-70-04:2014 (E) 5 Introduction The deleterious effects to be anticipated during the thermal cycling test under vacuum include: outgassing, cracking or fracture of materials or assemblies due to sudden dimensional changes by expansion, contraction or pressure, short c
22、ircuiting of electrical wiring, overheating of materials or assemblies due to change in convection and conductive heat transfer characteristics. BS EN 16602-70-04:2014EN 16602-70-04:2014 (E) 6 1 Scope This Standard establishes the requirements for the specification, the procedures, the execution and
23、 the reporting of a thermal cycling test under vacuum for the evaluation of materials, processes, mechanical parts and assemblies intended for use in the fabrication of spacecraft and associated equipment. This is one of the tests to determine the ability of theses articles to withstand changes of a
24、mbient temperature under vacuum. Typical materials or assemblies that can be evaluated by means of this test method are listed below. adhesives; adhesive bonded joints; coatings (paint, thermal and protective); insulating materials; metallic bonded joints; metallic samples, finished by plating or ch
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