DIN EN 16602-20-2014 Space product assurance - Quality assurance English version EN 16602-20 2014《航空产品保证 质量保证 英文版本EN 16602-20-2014》.pdf
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1、Dezember 2014DEUTSCHE NORM DIN-Normenausschuss Luft- und Raumfahrt (NL)Preisgruppe 24DIN Deutsches Institut fr Normung e. V. Jede Art der Vervielfltigung, auch auszugsweise, nur mit Genehmigung des DIN Deutsches Institut fr Normung e. V., Berlin, gestattet.ICS 49.140!% 38 5.8.6 38 5.8.7 38 5.8.8 Gen
2、eral requirements . 38 5.8.9 Maintenance . 39 6 Pre-tailoring matrix per space product types 40 Annex A (normative) QA plan - DRD 49 Annex B (normative) End item data package (EIDP) - DRD . 51 Annex C (normative) Logbook - DRD 53 Annex D (normative) Certificate of conformity (CoC) - DRD 55 Annex E (
3、informative) Example of a logbook cover page 57 Annex F (informative) Example of EIDP cover page 58 Annex G (informative) Example of EIDP contents 59 Annex H (informative) Example of Certificate of conformity . 60 Annex I (informative) QA document requirement list . 61 Annex J (informative) ECSS-Q-S
4、T-20 applicability according to programme phases . 62 Bibliography . 65 Tables Table I-1 : QA document requirement list with respect to milestones 61 Table J-1 : ECSS-Q-ST-20C Requirements per programme phase 62 DIN EN 16602-20:2014-12 EN 16602-20:2014 (E) 5 Foreword This document (EN 16602-20:2014)
5、 has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-20:2014) originates from ECSS-Q-ST-20C Rev.1. This European Standard shall be given the status of a national standard, either by publication of an identical text or by end
6、orsement, at the latest by March 2015, and conflicting national standards shall be withdrawn at the latest by March 2015.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 identif
7、ying any or all such patent rights. This document supersedes EN 13291-2:2003. 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 preced
8、ence 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 organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia,
9、 Cyprus, Czech 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 U
10、nited Kingdom. DIN EN 16602-20:2014-12 EN 16602-20:2014 (E) 6 1 Scope This Standard defines the quality assurance (QA) requirements for the establishment and implementation of a Quality Assurance programme for products of space projects. Discipline related qualification activities are complemented i
11、n standards specific to those disciplines (e.g. ECSS-E-ST-32-01 for fracture control). For software quality assurance, the software product assurance standard, ECSS-Q-ST-80 is applicable. This Standard is applicable to all space projects. This standard may be tailored for the specific characteristic
12、 and constrains of a space project in conformance with ECSS-S-ST-00. For the tailoring of this standard the following information is provided: A table providing the pre-tailoring per “Product types” in clause 6 A table providing the pre-tailoring per “Project phase” in Annex J DIN EN 16602-20:2014-1
13、2 EN 16602-20:2014 (E) 7 2 Normative references The following normative documents contain provisions which, through reference in this text, constitute provisions of this ECSS Standard. For dated references, subsequent amendments to, or revision of any of these publications do not apply. However, par
14、ties to agreements based on this ECSS Standard are encouraged to investigate the possibility of applying the more recent editions of the normative documents indicated below. For undated references, the latest edition of the publication referred to applies. EN reference Reference in text Title EN 166
15、01-00-01 ECSS-S-ST-00-01 ECSS system - Glossary of terms EN 16602-10 ECSS-Q-ST-10 Space product assurance - Product assurance management EN 16602-10-04 ECSS-Q-ST-10-04 Space product assurance - Critical-item control EN 16602-10-09 ECSS-Q-ST-10-09 Space product assurance - Nonconformance control syst
16、em EN 61340-5-1 (2007) Electrostatics - Part 5-1: Protection of electronic devices from electrostatic phenomena - General requirements ANSI-ESD S20.20-2007 Development of an Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts, Assemblies and Equipment DIN EN 166
17、02-20:2014-12 EN 16602-20:2014 (E) 8 3 Terms and definitions 3.1 Terms from other standards For the purpose of this Standard, the terms and definitions from ECSS-ST-00-01 apply, in particular for the following terms: nonconformance process product assurance quality assurance space system space segme
18、nt element space segment sub-system launch segment element launch segment sub-system ground segment element ground segment sub-system space segment equipment launch segment equipment ground segment equipment 3.2 Terms specific to the present standard 3.2.1 ground support equipment (GSE) optical, mec
19、hanical, fluidic, electrical and software support equipment or systems used for example for calibration, measurements, testing, simulation, transportation, and handling of space segment or of space segment elements 3.2.2 inspectability ability of an item of being inspected NOTE Inspectability includ
20、es provisions for the followings aspects: DIN EN 16602-20:2014-12 EN 16602-20:2014 (E) 9 Definition of inspection including acceptance or rejection criteria, expressed in an unambiguous and quantified manner. Part and component accessibility for inspection Definition of tolerance methods for dimensi
21、onal inspection performance (e.g. functional tolerances). 3.2.3 producibility ability of an item of being producible NOTE Producibility includes provisions for the following aspects: Design simplification and standardization, reduction in part types and part number. Guidelines for selection of prefe
22、rred parts, materials and processes. Unambiguous definitions of the requirements and limits to be used. Definition of tolerance build-up methods, in order to simplify manufacturing, assembly, inspection. Standardization of interfaces. Part accessibility for assembly and inspection. Definition of des
23、ign criteria consistent with the capability of manufacturing processes. Definition of design methods to ensure that the cleanliness requirements are compatible with the capability of related cleanliness procedures and facilities. 3.2.4 repeatability ability to reproduce the performance and character
24、istics of an item NOTE Repeatability includes provisions for the following aspects: Definition of standard tolerances generally applicable. Recommended design concepts and solutions to ensure repeatability. Recommended manufacturing processes having proven repeatability. Design criteria that optimiz
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