BS EN 16602-60-2015 Space product assurance Electrical electronic and electromechanical (EEE) components《航天产品保证 电气 电子和机电 (EEE) 元器件》.pdf

1、BSI Standards PublicationBS EN 16602-60:2015Space product assurance Electrical, electronic andelectromechanical (EEE)componentsBS EN 16602-60:2015 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 16602-60:2015.The UK participation in its preparation was entrusted

2、 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 the necessaryprovisions of a contract. Users are responsible for its correctapplication. The B

3、ritish Standards Institution 2015. Published by BSI StandardsLimited 2015ISBN 978 0 580 86647 0ICS 49.140Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 August

4、2015.Amendments issued since publicationDate Text affectedBS EN 16602-60:2015EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16602-60 August 2015 ICS 49.140 English version Space product assurance - Electrical, electronic and electromechanical (EEE) components Assurance produit des projets spat

5、iaux - Composants lectriques, lectroniques et lectromcaniques (EEE) Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) Bauteile This European Standard was approved by CEN on 16 November 2014. CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal R

6、egulations 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 such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN a

7、nd 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 CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status

8、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, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ir

9、eland, Italy, Latvia, Lithuania, 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 2015 CEN/CENELEC All rights of exploitation in any form and

10、by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16602-60:2015 EBS EN 16602-60:2015EN 16602-60:2015 (E) 2 Table of contents European foreword 7 Introduction 7 1 Scope . 9 2 Normative references . 10 3 Terms, definitions and abbreviated terms 12 3.1 Terms

11、from other standards 12 3.2 Terms specific to the present standard . 12 3.3 Abbreviated terms. 13 3.4 Conventions 15 3.5 Nomenclature . 16 4 Requirements for Class 1 components 17 4.1 Component programme management 17 4.1.1 General . 17 4.1.2 Components control programme . 17 4.1.3 Parts control boa

12、rd 17 4.1.4 Declared components list 18 4.1.5 Electrical and mechanical GSE . 19 4.2 Component selection, evaluation and approval . 19 4.2.1 General . 19 4.2.2 Manufacturer and component selection . 20 4.2.3 Component evaluation 22 4.2.4 Parts approval . 25 4.3 Component procurement 25 4.3.1 General

13、 . 25 4.3.2 Procurement specification . 26 4.3.3 Screening requirements 26 4.3.4 Initial customer source inspection (precap) . 27 4.3.5 Lot acceptance 27 4.3.6 Final customer source inspection (buy-off) 28 BS EN 16602-60:2015EN 16602-60:2015 (E) 3 4.3.7 Incoming inspections . 29 4.3.8 Radiation veri

14、fication testing . 29 4.3.9 Destructive physical analysis 30 4.3.10 Relifing 31 4.3.11 Manufacturers data documentation deliveries 31 4.4 Handling and storage 32 4.5 Component quality assurance 32 4.5.1 General . 32 4.5.2 Nonconformances or failures 32 4.5.3 Alerts. 33 4.5.4 Traceability . 33 4.5.5

15、Lot homogeneity for sampling test . 34 4.6 Specific components . 34 4.6.1 General . 34 4.6.2 ASICs 34 4.6.3 Hybrids 34 4.6.4 One time programmable devices . 34 4.6.5 Microwave monolithic integrated circuits . 35 4.7 Documentation . 35 5 Requirements for Class 2 components 37 5.1 Component programme

16、management 37 5.1.1 General . 37 5.1.2 Components control programme . 37 5.1.3 Parts Control Board . 37 5.1.4 Declared Components List 38 5.1.5 Electrical and mechanical GSE . 39 5.2 Component selection, evaluation and approval . 39 5.2.1 General . 39 5.2.2 Manufacturer and component selection . 40

17、5.2.3 Component evaluation 42 5.2.4 Parts approval . 44 5.3 Component procurement 45 5.3.1 General . 45 5.3.2 Procurement specification . 45 5.3.3 Screening requirements 46 5.3.4 Initial Customer Source Inspection (precap) 46 5.3.5 Lot acceptance 46 BS EN 16602-60:2015EN 16602-60:2015 (E) 4 5.3.6 Fi

18、nal customer source inspection (buy-off) 47 5.3.7 Incoming inspections . 47 5.3.8 Radiation verification testing . 48 5.3.9 Destructive physical analysis 49 5.3.10 Relifing 49 5.3.11 Manufacturers data documentation deliveries 50 5.4 Handling and storage 50 5.5 Component quality assurance 51 5.5.1 G

19、eneral . 51 5.5.2 Nonconformances or failures 51 5.5.3 Alerts. 51 5.5.4 Traceability . 51 5.5.5 Lot homogeneity for sampling test . 52 5.6 Specific components . 52 5.6.1 General . 52 5.6.2 ASICs 52 5.6.3 Hybrids 52 5.6.4 One time programmable devices . 52 5.6.5 Microwave monolithic integrated circui

20、ts . 53 5.7 Documentation . 53 6 Requirements for Class 3 components 55 6.1 Component programme management 55 6.1.1 General . 55 6.1.2 Components control programme . 55 6.1.3 Parts control board 55 6.1.4 Declared components list 55 6.1.5 Electrical and mechanical GSE . 56 6.2 Component selection, ev

21、aluation and approval . 56 6.2.1 General . 56 6.2.2 Manufacturer and component selection . 57 6.2.3 Component evaluation 59 6.2.4 Parts approval . 61 6.3 Component procurement 62 6.3.1 General . 62 6.3.2 Procurement specification . 62 6.3.3 Screening requirements 63 6.3.4 Initial customer source ins

22、pection (precap) . 63 BS EN 16602-60:2015EN 16602-60:2015 (E) 5 6.3.5 Lot acceptance 63 6.3.6 Final customer source inspection (buy-off) 64 6.3.7 Incoming inspections . 64 6.3.8 Radiation verification testing . 65 6.3.9 Destructive physical analysis 65 6.3.10 Relifing 66 6.3.11 Manufacturers data do

23、cumentation deliveries 66 6.4 Handling and storage 66 6.5 Component quality assurance 67 6.5.1 General . 67 6.5.2 Nonconformances or failures 67 6.5.3 Alerts. 68 6.5.4 Traceability . 68 6.5.5 Lot homogeneity for sampling test . 68 6.6 Specific components . 68 6.6.1 Overview . 68 6.6.2 ASICs 68 6.6.3

24、 Hybrids 69 6.6.4 One time programmable devices . 69 6.6.5 Microwave monolithic integrated circuits . 70 6.7 Documentation . 70 7 Quality levels 72 Annex A (normative) Component control plan (CCP) - DRD . 86 Annex B (normative) Declared component list (DCL) - DRD . 88 Annex C (normative) Procurement

25、 specification - DRD 90 Annex D (normative) Part approval document (PAD) - DRD . 92 Annex E (informative) EEE documents delivery per review 95 Bibliography . 98 Tables Table 4-1: Document requirements list for Class 1 components . 36 Table 5-1: Document requirements list for Class 2 components . 54

26、Table 6-1:Document requirements list for Class 3 components 71 Table 7-1: Quality levels for Class 1 components 72 Table 7-2: Quality levels for Class 2 components . 76 BS EN 16602-60:2015EN 16602-60:2015 (E) 6 Table 7-3: Quality levels for Class 3 components . 81 Table D-1 : PAD sheet 93 Table E-1

27、: EEE delivery documents 96 BS EN 16602-60:2015EN 16602-60:2015 (E) 7 European foreword This document (EN 16602-60:2015) has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-60:2015) originates from ECSS-Q-ST-60C Rev.2. This

28、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 February 2016, and conflicting national standards shall be withdrawn at the latest by February 2016. Attention is drawn to the possibility that some of t

29、he 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 Free Trade Association. This docu

30、ment 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 organizations of the following countries

31、 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, Malta, Netherlands, Norway, Poland,

32、 Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 16602-60:2015EN 16602-60:2015 (E) 8 Introduction The objective of the EEE component selection, control, procurement and use requirements is to ensure that EEE components used in a space project e

33、nables the project to meet its mission requirements. Important elements of EEE component requirements include: a. component programme management, b. component selection, evaluation and approval, c. procurement, d. handling and storage, e. component quality assurance, f. specific components, and g. d

34、ocumentation. The main tools which can be used to reach the objective are: a. concurrent engineering, b. standardization of component types, c. characterization of components, d. assessment of component manufacturers including declared competencies and processes, e. testing, screening, lot acceptanc

35、e and periodic testing, f. procurement specifications, g. control and inspection, h. control of nonconforming materials, i. assessment and use of existing component data, j. application of specific control to mitigate risk for components with limited data or confidence, and k. information management

36、. The basic approach is as follows: The customer of a given space project defines the EEE component requirements within the boundaries of this standard. They appear in the appropriate clauses of the project requirements as defined in ECSS-M-ST-10. The supplier defines a component control plan to imp

37、lement those requirements into a system which enables, for instance, to control the selection, approval, procurement, handling in a schedule compatible with his requirements, and in a cost-efficient way. The supplier ensures that the applicable parts requirements are passed down to lower level suppl

38、iers and ensure that they are compliant to these parts requirements. BS EN 16602-60:2015EN 16602-60:2015 (E) 9 1 Scope This European Standard defines the requirements for selection, control, procurement and usage of EEE components for space projects. This standard differentiates between three classe

39、s of components through three different sets of standardization requirements (clauses) to be met. The three classes provide for three levels of trade-off between assurance and risk. The highest assurance and lowest risk is provided by class 1 and the lowest assurance and highest risk by class 3. Pro

40、curement costs are typically highest for class 1 and lowest for class 3. Mitigation and other engineering measures may decrease the total cost of ownership differences between the three classes. The project objectives, definition and constraints determine which class or classes of components are app

41、ropriate to be utilised within the system and subsystems. a. Class 1 components are described in Clause 4. b. Class 2 components are described in Clause 5 c. Class 3 components are described in Clause 6. The requirements of this document apply to all parties involved at all levels in the integration

42、 of EEE components into space segment hardware and launchers. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00. BS EN 16602-60:2015EN 16602-60:2015 (E) 10 2 Normative references The following normative documents contai

43、n 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, parties to agreements based on this ECSS Standard are encouraged to investigate the possibi

44、lity 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 16601-00-01 ECSS-S-ST-00-01 ECSS system Glossary of terms EN 16601-10 ECSS-M-ST-10 Space pr

45、oject management Project planning and implementation EN 16602-10-09 ECSS-Q-ST-10-09 Space product assurance Nonconformance control system EN 16602-20 ECSS-Q-ST-20 Space product assurance Quality assurance EN 16602-30-11 ECSS-Q-ST-30-11 Space product assurance Derating EEE components EN 16602-60-02 E

46、CSS-Q-ST-60-02 Space product assurance ASIC and FPGA development EN 16602-60-05 ECSS-Q-ST-60-05 Space product assurance Generic procurement requirements for hybrid microcircuits EN 16602-60-12 ECSS-Q-ST-60-12 Space product assurance Design, selection, procurement and use of die form monolithic micro

47、wave integrated circuits (MMICs) EN 16602-60-13 ECSS-Q-ST-60-13 Commercial electrical, electronic and electromechanical (EEE) components EN 16602-60-14 ECSS-Q-ST-60-14 Space product assurance Relifing procedure EEE components EN 16602-60-15 ECSS-Q-ST-60-15 Radiation hardness assurance EEE components

48、 EN 16602-70 ECSS-Q-ST-70 Space product assurance Materials, mechanical parts and processes ESCC 20200 ESCC: Component Manufacturer Evaluation ESCC 22800 ESCC: ESA/SCC Non conformance Control System ESCC 22900 ESCC Basic Specification: Total Dose Steady-State BS EN 16602-60:2015EN 16602-60:2015 (E)

49、11 EN reference Reference in text Title Irradiation Test Method ESCC 24900 Minimum requirements for controlling environmental contamination of components ESCC 25500 Methodology for the detection of pure tin in the external surface finish of case and leads of EEE components ESCC QPL ESCC qualified part list (https:/escies.org) ESCC EPPL ESCC European preferred parts list (https:/escies.org) ESCC QML ESCC qualified manufacturers list (https:/escies.org) MIL QPLs MIL qualified parts lists MIL QMLs MIL qualified manufacturers lists NPSL NASA Parts