SIST EN 16602-60:2015
(Main)Space product assurance - Electrical, electronic and electromechanical (EEE) components
Space product assurance - Electrical, electronic and electromechanical (EEE) components
This standard defines the requirements for selection, control, procurement and usage of EEE components for space projects.
This standard differentiates between three classes 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. Procurement 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 appropriate 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 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.
Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) Bauteile
Assurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)
Zagotavljanje varnih proizvodov v vesoljski tehniki - Električne, elektronske in elektromehanske komponente
Ta standard določa zahteve za izbiro, nadzor, nabavo in uporabo električnih, elektronskih in elektromehanskih komponent (EEE) v vesoljski tehniki. Ta standard razlikuje med tremi razredi komponent s pomočjo treh različnih naborov standardizacijskih zahtev (določil), ki morajo biti izpolnjene. Ti trije razredi določajo tri ravni kompromisov med zagotovili in tveganjem. Največje zagotovilo in najmanjše tveganje zagotavlja razred 1, najmanjše zagotovilo in največje tveganje pa razred 3. Stroški nabave so običajno najvišji za razred 1 in najnižji za razred 3. Ukrepi za blažitev in drugi inženirski ukrepi lahko zmanjšajo skupne stroške lastniških razlik med temi tremi razredi. Cilji projekta, njegova opredelitev in omejitve določajo, kateri razred ali razredi komponent so ustrezni za uporabo v sistemu in podsistemih. a. Komponente razreda 1 so opisane v točki 4. b. Komponente razreda 2 so opisane v točki 5 c. Komponente razreda 3 so opisane v točki 6. Zahteve tega dokumenta veljajo za vse vpletene strani na vseh ravneh integracije električnih, elektronskih in elektromehanskih komponent v vesoljski strojni opremi in lansirnikih. Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.
General Information
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) BauteileAssurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)Space product assurance - Electrical, electronic and electromechanical (EEE) components49.140Vesoljski sistemi in operacijeSpace systems and operations49.060Aerospace electric equipment and systemsICS:Ta slovenski standard je istoveten z:EN 16602-60:2015SIST EN 16602-60:2015en,fr,de01-oktober-2015SIST EN 16602-60:2015SLOVENSKI
STANDARD
SIST EN 16602-60:2015
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16602-60
August 2015 ICS 49.140
English version
Space product assurance - Electrical, electronic and electromechanical (EEE) components
Assurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (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 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 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 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, 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 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 for CEN national Members and for CENELEC Members. Ref. No. EN 16602-60:2015 E SIST EN 16602-60:2015
EN 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 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 board . 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 . 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 SIST EN 16602-60:2015
EN 16602-60:2015 (E) 3 4.3.7 Incoming inspections . 29 4.3.8 Radiation verification testing . 29 4.3.9 Destructive physical analysis . 30 4.3.10 Relifing . 31 4.3.11 Manufacturer’s 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 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 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 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 SIST EN 16602-60:2015
EN 16602-60:2015 (E) 4 5.3.6 Final 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 Manufacturer’s data documentation deliveries . 50 5.4 Handling and storage . 50 5.5 Component quality assurance . 51 5.5.1 General . 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 circuits . 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, evaluation 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 inspection (precap) . 63 SIST EN 16602-60:2015
EN 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 Manufacturer’s data documentation 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 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 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 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 SIST EN 16602-60:2015
EN 16602-60:2015 (E) 6 Table 7-3: Quality levels for Class 3 components . 81 Table D-1 : PAD sheet. 93 Table E-1 : EEE delivery documents . 96
SIST EN 16602-60:2015
EN 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 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 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 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 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 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 Kingdom. SIST EN 16602-60:2015
EN 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 enables 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. documentation. 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 acceptance 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. 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 implement 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 suppliers and ensure that they are compliant to these parts requirements. SIST EN 16602-60:2015
EN 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 classes 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. Procurement 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 appropriate 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 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. SIST EN 16602-60:2015
EN 16602-60:2015 (E) 10 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, 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 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 project 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 ECSS-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 microwave 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 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 SIST EN 16602-60:2015
EN 16602-60:2015 (E) 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 Selection List
JAXA QPL JAXA qualified parts list
ESCC, MIL & JAXA specifications and standards called in the document
SIST EN 16602-60:2015
EN 16602-60:2015 (E) 12 3 Terms, definitions and abbreviated terms 3.1 Terms from other standards For the purpose of this Standard, the terms and definitions from ECSS-S-ST-00-01 apply. 3.2 Terms specific to the present standard 3.2.1 agent organization contracted to perform the procurement of EEE components including related engineering and quality assurance tasks 3.2.2 characterization determination of the attributes of an EEE component, in sufficient detail to allow assessment of its suitability for a particular use or application
3.2.3 commercial component part neither designed, nor manufactured with reference to military or space standards
3.2.4 concurrent engineering engineering activity taking place in the context of simultaneous design of the product, the production process and all associated product usages, in an integrated, multifunctional team, with external organizational constraints minimized 3.2.5 destructive physical analysis series of inspections, tests and analyses performed on a sample of components to verify that the material, design and workmanship used for its construction, as well as the construction itself, meet the requirements of the relevant specification and are suitable for the intended application 3.2.6 franchised distributor distributor officially and contractually authorised by the manufacturer 3.2.7 parts engineer professional engineer with demonstratable specialisation in EEE components SIST EN 16602-60:2015
EN 16602-60:2015 (E) 13 3.2.8 parts procurer supplier who procures components by himself or a parts procurement agent who procures parts for the supplier 3.2.9 qualified parts parts belonging to QPLs or QMLs from the following normative systems: ESCC, MIL, JAXA, CECC 3.2.10 screening tests, inspections or combination thereof, imposed on 100% of parts, to remove unsatisfactory items or those likely to exhibit early failures 3.2.11 space qualified parts parts belonging to QPLs or QMLs from the following normative systems (ESCC, MIL) according to quality levels listed in Table 7-1
NOTE 1 Space qualified parts are a subset of the qualified parts defined in clause 3.2.9. NOTE 2 Parts belonging to JAXA QPL are considered as space qualified provided the equivalence of the generic JAXA specification with the ESCC or MIL generic specifications has been established. 3.3 Abbreviated terms For the purpose of this Standard, the abbreviated terms from ECSS-S-ST-00-01 and the following apply: Abbreviation Meaning ASIC Application specific integrated circuit CCD charge coupled device CCP Component control plan CDR critical design review CECC CENELEC electronic components committee CENELEC Comité Européen de Normalisation Electrotechnique CI
conformance inspection CN change notice CoC certificate of conformance CPPA centralized parts procurement agent CR change request CSI customer source inspection CSV comma-separated values DCL declared components list DPA destructive physical analysis DRD document requirement definition EEE electrical, electronic, electromechanical SIST EN 16602-60:2015
EN 16602-60:2015 (E) 14 EFR established failure rate EPPL European preferred parts list ESCC European space components coordination ESR equivalent serial resistance FPGA field programmable gate arrays GSE ground support equipment GSFC Goddard space flight center JAXA Japanese aerospace exploration agency JD justification document LAT lot acceptance test LED light emitting diode LVT lot validation testing MMIC microwave monolithic integrated circuit NASA national aeronautics and space administration NCR nonconformance report NPSL NASA parts selection list PA product assurance PAD part approval document PCB parts control board PCN process change notice PDR preliminary design review PIND particle impact noise detection QCI quality conformance inspection QML qualified manufacturers list QPL qualified parts list RFD request for deviation RFW request for waiver RVT radiation verification testing SCSB Space Components Steering Board SEB single event burn-out SEE single event effect SEFI single event functional interrupt SEGR single event gate rupture SEL single event latch-up SET single event transient SEU single event upset TCI technology conformance inspection TRR test readiness review
WFR W
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) BauteileAssurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)Space product assurance - Electrical, electronic and electromechanical (EEE) components49.140Vesoljski sistemi in operacijeSpace systems and operations49.060Aerospace electric equipment and systemsICS:Ta slovenski standard je istoveten z:FprEN 16602-60kSIST FprEN 16602-60:2014en,fr,de01-julij-2014kSIST FprEN 16602-60:2014SLOVENSKI
STANDARD
kSIST FprEN 16602-60:2014
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
FINAL DRAFT
FprEN 16602-60
May 2014 ICS 49.140
English version
Space product assurance - Electrical, electronic and electromechanical (EEE) components
Assurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)
Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) Bauteile This draft European Standard is submitted to CEN members for unique acceptance procedure. It has been drawn up by the Technical Committee CEN/CLC/TC 5.
If this draft becomes a European Standard, 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.
This draft European Standard was established by CEN and CENELEC 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 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, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are aware and to provide supporting documentation.
Warning : This document is not a European Standard. It is distributed for review and comments. It is subject to change without notice and shall not be referred to as a European Standard. 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 worldwide for CEN national Members and for CENELEC Members. Ref. No. FprEN 16602-60:2014 E kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 2 Table of contents Foreword . 7 Introduction . 8 1 Scope . 9 2 Normative references . 10 3 Terms, definitions and abbreviated terms . 12 3.1 Terms 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 board . 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 . 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 kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 3 4.3.7 Incoming inspections . 29 4.3.8 Radiation verification testing . 29 4.3.9 Destructive physical analysis . 30 4.3.10 Relifing . 31 4.3.11 Manufacturer’s 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 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 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 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 kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 4 5.3.6 Final 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 Manufacturer’s data documentation deliveries . 50 5.4 Handling and storage . 50 5.5 Component quality assurance . 51 5.5.1 General . 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 circuits . 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, evaluation 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 inspection (precap) . 63 kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (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 Manufacturer’s data documentation 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 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 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 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 kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 6 Table 7-3: Quality levels for Class 3 components . 81 Table D-1 : PAD sheet. 93 Table E-1 : EEE delivery documents . 96
kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 7 Foreword This document (FprEN 16602-60:2014) has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN (Germany). This document (FprEN 16602-60:2014) originates from ECSS-Q-ST-60C Rev.2. This document is currently submitted to the Unique Acceptance Procedure. This document has been developed to cover specifically space systems and will the-refore have precedence over any EN covering the same scope but with a wider do-main of applicability (e.g. : aerospace). kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (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 enables 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. documentation. 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 acceptance 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. 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 implement 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 suppliers and ensure that they are compliant to these parts requirements. kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 9 1 Scope This standard defines the requirements for selection, control, procurement and usage of EEE components for space projects. This standard differentiates between three classes 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. Procurement 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 appropriate 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 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. kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 10 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, 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 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 project 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 ECSS-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 microwave 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 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 kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 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 Selection List
JAXA QPL JAXA qualified parts list
ESCC, MIL & JAXA specifications and standards called in the document
kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 12 3 Terms, definitions and abbreviated terms 3.1 Terms from other standards For the purpose of this Standard, the terms and definitions from ECSS-S-ST-00-01 apply. 3.2 Terms specific to the present standard 3.2.1 agent organization contracted to perform the procurement of EEE components including related engineering and quality assurance tasks 3.2.2 characterization determination of the attributes of an EEE component, in sufficient detail to allow assessment of its suitability for a particular use or application
3.2.3 commercial component part neither designed, nor manufactured with reference to military or space standards
3.2.4 concurrent engineering engineering activity taking place in the context of simultaneous design of the product, the production process and all associated product usages, in an integrated, multifunctional team, with external organizational constraints minimized 3.2.5 destructive physical analysis series of inspections, tests and analyses performed on a sample of components to verify that the material, design and workmanship used for its construction, as well as the construction itself, meet the requirements of the relevant specification and are suitable for the intended application 3.2.6 franchised distributor distributor officially and contractually authorised by the manufacturer 3.2.7 parts engineer professional engineer with demonstratable specialisation in EEE components kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 13 3.2.8 parts procurer supplier who procures components by himself or a parts procurement agent who procures parts for the supplier 3.2.9 qualified parts parts belonging to QPLs or QMLs from the following normative systems: ESCC, MIL, JAXA, CECC 3.2.10 screening tests, inspections or combination thereof, imposed on 100% of parts, to remove unsatisfactory items or those likely to exhibit early failures 3.2.11 space qualified parts parts belonging to QPLs or QMLs from the following normative systems (ESCC, MIL) according to quality levels listed in Table 7-1
NOTE 1 Space qualified parts are a subset of the qualified parts defined in clause 3.2.9. NOTE 2 Parts belonging to JAXA QPL are considered as space qualified provided the equivalence of the generic JAXA specification with the ESCC or MIL generic specifications has been established. 3.3 Abbreviated terms For the purpose of this Standard, the abbreviated terms from ECSS-S-ST-00-01 and the following apply: Abbreviation Meaning ASIC Application specific integrated circuit CCD charge coupled device CCP Component control plan CDR critical design review CECC CENELEC electronic components committee CENELEC Comité Européen de Normalisation Electrotechnique CI
conformance inspection CN change notice CoC certificate of conformance CPPA centralized parts procurement agent CR change request CSI customer source inspection CSV comma-separated values DCL declared components list DPA destructive physical analysis DRD document requirement definition EEE electrical, electronic, electromechanical kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 14 EFR established failure rate EPPL European preferred parts list ESCC European space components coordination ESR equivalent serial resistance FPGA field programmable gate arrays GSE ground support equipment GSFC Goddard space flight center JAXA Japanese aerospace exploration agency JD justification document LAT lot acceptance test LED light emitting diode LVT lot validation testing MMIC microwave monolithic integrated circuit NASA national aeronautics and space administration NCR nonconformance report NPSL NASA parts selection list PA product assurance PAD part approval document PCB parts control board PCN process change notice PDR preliminary design review PIND particle impact noise detection QCI quality conformance inspection QML qualified manufacturers list QPL qualified parts list RFD request for deviation RFW request for waiver RVT radiation verification testing SCSB Space Components Steering Board SEB single event burn-out SEE single event effect SEFI single event functional interrupt SEGR single event gate rupture SEL single event latch-up SET single event transient SEU single event upset TCI technology conformance inspection TRR test readiness review
WFR Weibull failure rate kSIST FprEN 16602-60:2014
FprEN 16602-60:2014 (E) 15 3.4 Conventions a. The term “EEE component“ is synonymous with the terms "EEE Part", "Component" or just "Part". b. The term “for approval” means that a decision of the approval authority is necessary for continuing the process.
c. The term “for review” means that raised reviewers comments are considered and dispositioned. d. The term “for information” means that no comments are expected about
the delivered item. e. For the purpose of clear understanding of this document, hereunder is a
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