BS EN 16602-60-13-2015 Space product assurance Requirements for the use of COTS components《航天产品保证 COTS元器件的使用要求》.pdf

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1、BSI Standards PublicationBS EN 16602-60-13:2015Space product assurance Requirements for the use ofCOTS componentsBS EN 16602-60-13:2015 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN16602-60-13:2015.The UK participation in its preparation was entrusted to Techn

2、icalCommittee 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 British St

3、andards Institution 2015. Published by BSI StandardsLimited 2015ISBN 978 0 580 86646 3ICS 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 2015.Amen

4、dments issued since publicationDate Text affectedBS EN 16602-60-13:2015EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16602-60-13 August 2015 ICS 49.140 English version Space product assurance - Requirements for the use of COTS components Assurance produit des projets spatiaux - Exigences pour

5、 lutilisation de composants commerciaux sur tagre Raumfahrtproduktsicherung - Anforderungen fr die Nutzung von COTS-Komponenten This European Standard was approved by CEN on 16 November 2014. CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the co

6、nditions 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 European

7、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. CEN and

8、 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, Lithuania,

9、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 by any means reserved worldwide f

10、or CEN national Members and for CENELEC Members. Ref. No. EN 16602-60-13:2015 EBS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 2 Table of contents European foreword 4 Introduction 4 1 Scope . 7 2 Normative references . 9 3 Terms, definitions and abbreviated terms 11 3.1 Terms from other standards 11 3

11、.2 Terms specific to the present standard . 11 3.3 Abbreviated terms. 12 3.4 Conventions 13 3.5 Nomenclature . 14 4 Requirements for class 1 components . 15 5 Requirements for class 2 components . 36 6 Requirements for class 3 components . 59 7 Quality levels 74 8 Evaluation and lot acceptance for r

12、etinned parts 75 9 Pure tin lead finish risk analysis 83 Annex A (normative) Component control plan (CCP) - DRD . 84 Annex B (normative) Declared components list (DCL) - DRD . 85 Annex C (normative) Internal Suppliers specification - DRD . 86 Annex D (normative) Parts approval document - DRD 88 Anne

13、x E (informative) EEE documents delivery per review 89 Annex F (normative) Justification document - DRD 90 Annex G (informative) Difference between the three classes . 93 Annex H (informative) Flow chart for construction analysis and destructive physical analysis . 94 BS EN 16602-60-13:2015EN 16602-

14、60-13:2015 (E) 3 Bibliography . 98 Figures Figure 4-1: Evaluation tests flow chart for Class 1 components 21 Figure 4-2: Lot acceptance tests flow chart for Class 1 components 28 Figure 5-1: Evaluation Tests flow charts for Class 2 components . 42 Figure 5-2: Lot acceptance tests flow chart for Clas

15、s 2 components 51 Figure 6-1: Lot acceptance test flow chart for Class 3 components 67 Figure 8-1: Evaluation flow chart for retinned parts class 1 programmes . 76 Figure 8-2: Lot acceptance flow chart for retinned parts class 1 programmes . 77 Figure 8-3: Evaluation flow chart for retinned parts cl

16、ass 2 programmes . 79 Figure 8-4: Lot acceptance flow chart for retinned parts class 2 programmes . 80 Figure 8-5: Evaluation flow chart for retinned parts class 3 programmes . 81 Figure 8-6: Lot acceptance flow chart for retinned parts class 3 programmes . 82 Tables Table 4-1: Evaluation Tests for

17、Class 1 components 21 Table 4-2: Screening tests for Class 1 components 25 Table 4-3: Lot acceptance tests for Class 1 components 29 Table 4-4: Documentation for Class 1 components 35 Table 5-1: Evaluation Tests for Class 2 components 43 Table 5-2: Screening tests for the Class 2 components 48 Table

18、 5-3: Lot acceptance tests for Class 2 components 52 Table 5-4: Documentation for Class 2 components 58 Table 6-1: Evaluation tests for Class 3 components . 63 Table 6-2: Screening tests for Class 3 components 65 Table 6-3: Lot acceptance tests for Class 3 components 68 Table 6-4: Documentation for

19、Class 3 components 73 Table H-1 : Construction analysis and DPA 94 Table H-2 : Construction analysis sequence . 95 Table H-3 : Destructive physical analysis sequence . 97 BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 4 European foreword This document (EN 16602-60-13:2015) has been prepared by Techni

20、cal Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-60-13:2015) originates from ECSS-Q-ST-60-13C. 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 F

21、ebruary 2016, and conflicting national standards shall be withdrawn at the latest by February 2016. 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 or all such p

22、atent rights. 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 any EN covering the same scope but with a wider domain

23、 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, Czech Republic, Denmark, Estonia, Finland, Former Yugos

24、lav 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 Kingdom. BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 5 I

25、ntroduction This European Standard is based on and complementary to ECSS-Q-ST-60C (with upward revisions). This standard can only be used in conjunction with ECSS-Q-ST-60C in its current revision. This standard applies only to commercial components - as defined in its scope - which meet defined tech

26、nical parameters that are on the system application level demonstrated to be unachievable with existing space components or only achievable with qualitative and quantitative penalties. The standard requires that qualitative and quantitative penalties are specified, as applicable, as a minimum in ter

27、ms of quantifiable parameters such as: functional capability, parts count, power dissipation, frequency of operation, data/signal processing efficiency, interconnect complexity, mass, volume, For traceability to ECSS-Q-ST-60, the modifications or additions are marked in blue. Text in black colour is

28、 unmodified text. The objective of the EEE component selection, control, procurement and use requirements is to ensure that EEE components used in a space project enables the project to meet its mission requirements. Important elements of EEE component requirements include: a. component programme ma

29、nagement, b. component selection, evaluation and approval, c. procurement, d. handling and storage, e. component quality assurance, f. specific components, and g. documentation. The main tools which can be used to reach the objective are: a. concurrent engineering, b. standardization of component ty

30、pes, c. characterization of components, d. assessment of component manufacturers including declared competencies and processes, e. testing, screening, lot acceptance and periodic testing, f. procurement specifications, g. control and inspection, h. control of nonconforming materials, i. assessment a

31、nd use of existing component data, j. application of specific control to mitigate risk for components with limited data or confidence, and BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 6 k. information management. The basic approach is as follows: The customer of a given space project defines the EE

32、E 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 implement those requirements into a system which enables, for instance, to control the sele

33、ction, 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 suppliers and ensure that they are compliant to these parts requirements. BS EN 16602-60-13:2

34、015EN 16602-60-13:2015 (E) 7 1 Scope This standard defines the requirements for selection, control, procurement and usage of EEE commercial components for space projects. This standard is applicable to commercial encapsulated active monolithic parts (integrated circuits and discrete): diodes microwa

35、ve diodes integrated circuits microwave integrated circuits (MMIC) transistors microwave transistors This standard is not applicable to the commercial parts from the following families: capacitors connectors crystals filters fuses heaters inductors microwave passive parts oscillators relays resistor

36、s switches thermistors transformers cables & wires hybrids surface acoustic waves (SAW) charge coupled devices (CCD) active pixel sensors (APS) BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 8 In addition, the following families of EEE components are not addressed by the present ECSS standard but it

37、can be used as guideline and revisited on case/case basis: photodiodes light emitting diodes (LED) phototransistors opto-couplers laser diodes In line with ECSS-Q-ST-60, this standard differentiates between three classes of components through three different sets of standardization requirements (cla

38、uses) 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. Procurement costs are typically highest for class 1 and lowest for class 3. Mitigati

39、on and other engineering measures can 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 appropriate to be utilised within the system and subsystems. a. Class 1 components a

40、re described in Clause 4 b. Class 2 components are described in Clause 5 c. Class 3 components are described in Clause 6 Annex G includes a diagram that summarizes the difference between these three classes for evaluation, screening and lot acceptance. The requirements of this document are applicabl

41、e to all parties involved at all levels in the integration of EEE commercial components into space segment hardware and launchers. For easy tailoring and implementation of the requirements into a Requirement Management Tool, and for direct traceability to ECSS-Q-ST-60, requirements in this standards

42、 have been written in the way of a ECSS Applicability Requirement Matrix (EARM), as defined in Annex A of ECSS-S-ST-00 “ECSS system Description, implementation and general requirements”. This standard may be tailored for the specific characteristics and constrains of a space project in conformance w

43、ith ECSS-S-ST-00. BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 9 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 thes

44、e publications do not apply. However, parties 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

45、 reference Reference in text Title EN 16601-00-01 ECSS-S-ST-00-01 ECSS system - Glossary of terms EN 16602-60 ECSS-Q-ST-60 Space product assurance - Electrical, electronic and electromechanical (EEE) components EN 16602-60-14 ECSS-Q-ST-60-14 Space product assurance - Relifing procedure - EEE compone

46、nts EN 16602-60-15 ECSS-Q-ST-60-15 Space product assurance Radiation hardness assurance EEE components ESCC 21300 Terms, definitions, abbreviations, symbols and units ESCC 24900 Minimum requirements for controlling environmental contamination of components ESCC 25500 Methodology for the detection of

47、 pure tin in the external surface finish of case and leads of EEE components MIL-STD-750 Test methods for semiconductor devices MIL-STD-883 Test method standard microcircuits JESD22-A101 Steady state temperature humidity bias life test JESD22-A110 Highly accelerated temperature and humidity stress t

48、est JESD22-A113 Preconditioning of plastic surface mount devices prior to reliability testing JESD22-A121 Test Method for Measuring Whisker Growth on Tin and Tin Alloy Surface Finishes JESD22-B106 Resistance to soldering temperature for through hole mounted devices JESD-201 Environmental Acceptance

49、Requirements for Tin BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 10 Whisker Susceptibility of Tin and Tin Alloy Surface Finishes J-STD-020 Moisture/Reflow sensitivity classification for nonhermetic solid state surface mount devices J-STD-033 Handling, packing, shipping and use of moisture/ reflow sensitive surface mount devices BS EN 16602-60-13:2015EN 16602-60-13:2015 (E) 11 3 Terms, definitions and abbreviated terms 3.1 Terms from other standards For the purpose of this standard, the terms