1、November 2015DEUTSCHE NORM DIN-Normenausschuss Luft- und Raumfahrt (NL)Preisgruppe 31DIN 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!%E?“2342899www.din.deDDIN EN 166
2、02-60-13Raumfahrtproduktsicherung Anforderungen fr die Nutzung von COTS-Komponenten;Englische Fassung EN 16602-60-13:2015Space product assurance Requirements for the use of COTS components;English version EN 16602-60-13:2015Assurance produit des projets spatiaux Exigences pour lutilisation de compos
3、ants commerciaux sur tagre;Version anglaise EN 16602-60-13:2015Alleinverkauf der Normen durch Beuth Verlag GmbH, 10772 Berlin www.beuth.deGesamtumfang 104 SeitenDIN EN 16602-60-13:2015-11 2 Nationales Vorwort Dieses Dokument (EN 16602-60-13:2015) wurde vom Technischen Komitee CEN/CLC/TC 5 Raumfahrt“
4、 erarbeitet, dessen Sekretariat vom DIN (Deutschland) gehalten wird. Das zustndige deutsche Normungsgremium ist der Arbeitsausschuss NA 131-06-02 AA Interoperabilitt von Informations-, Kommunikations- und Navigationssystemen“ im DIN-Normenausschuss Luft- und Raumfahrt (NL). Dieses Dokument (EN 16602
5、-60-13:2015) basiert auf ECSS-Q-ST-60-13C. Dieses Dokument enthlt unter Bercksichtigung des DIN-Prsidialbeschlusses 1/2004 nur die englische Originalfassung von EN 16602-60-13:2015. Dieses Dokument wurde speziell zur Behandlung von Raumfahrtsystemen erarbeitet und hat daher Vorrang vor jeglicher Eur
6、opischer Norm, da es denselben Anwendungsbereich hat, jedoch ber einen greren Geltungsbereich (z. B. Luft- und Raumfahrt) verfgt. DIN EN 16602-60-13:2015-11 3 Nationaler Anhang NA (informativ) Begriffe und Abkrzungen 3 Begriffe und Abkrzungen 3.1 Begriffe aus anderen Normen Fr die Anwendung dieser N
7、orm gelten die Begriffe nach ECSS-S-ST-00-01. Fr die Anwendung dieser Norm gelten die folgenden Begriffe nach ECSS-Q-ST-60: Agent Charakterisierung handelsbliche Komponente simultane Entwicklung Franchiseverteiler Teileentwickler Teilebeschaffer qualifizierte Teile Kontrolle fr die Raumfahrt qualifi
8、zierte Teile 3.2 Fr diese Norm spezifische Begriffe 3.2.1 Rckverfolgbarkeitsinformationen Rckverfolgungscode unverwechselbarer Kennzeichner, der von Herstellern dazu verwendet wird, eine Menge von Komponenten mit einer gemeinsamen Herstellungsgeschichte und dementsprechend gemeinsamen Charakteristik
9、en zu kennzeichnen und zurckzuverfolgen ANMERKUNG 1 Der Begriff Lot von EEE-Teilen“, der fr die Abstrahlung und Lotannahme verwendet wird, wird durch den Rckverfolgungscode definiert. ANMERKUNG 2 Es knnen mehrere Rckverfolgungscodes Teil derselben Lieferung vom Hersteller oder Vertreiber sein. ANMER
10、KUNG 3 Es ist mglich, verschiedene Diffusionslose (nach ESCC 21300) unter demselben Rckverfolgungs-code zusammenzufassen. DIN EN 16602-60-13:2015-11 4 3.3 Abkrzungen Fr die Anwendung dieser Norm gelten die Abkrzungen in ECSS-S-ST-00-01 und die folgenden Abkrzungen: Abkrzung Bedeutung AOQ durchschnit
11、tliche Ausgangsqualitt (en: average outgoing quality) ASIC anwendungsspezifischer integrierter Schaltkreis (en: application specific integrated circuit) BGA Kugelgitteranordnung (en: ball grid array) CA Konstruktionsanalyse (en: construction analysis) CCD ladungsgekoppeltes Bauelement (en: charge co
12、upled device) CCP Bauteilkontrollplan (en: component control plan) CN nderungsbenachrichtigung (en: change notice) CoC Konformittszertifikat (en: certificate of conformance) CDR kritische Entwurfsprfung (en: critical design review ) CR nderungsanforderung (en: change request) DCL deklarierte Kompone
13、ntenliste (en: declared components list) DPA destruktive physische Analyse (en: destructive physical analysis) DRD Dokumentenanforderungsdefinition (en: document requirement definition) DSM tiefe Submikron (en: deep Sub-Micron) Ea Auslsungsenergie (en: activation energy) ECSS Europische Kooperation
14、fr Raumfahrtnormung (en: European Coordination for Space Standardization) EEE elektrisch, elektronisch, elektromechanisch (en: electrical, electronic, electromechanical) EFR frhe Misserfolgsrate (en: early failure rate) ESCC Europische Raumfahrtkomponentenkoordination (en: European space components
15、coordination) GSE Bodenuntersttzungsausrstung (en: ground support equipment) HAST Hochbeschleunigter Belastungstest (en: highly accelerated stress test) HTRB Hochtemperatur-Sperrvorspannung (en: high temperature reverse bias) JD Rechtfertigungsdokument (en: justification document) DIN EN 16602-60-13
16、:2015-11 5 Abkrzung Bedeutung LAT Losannahmetest (en: lot acceptance test) LED Leuchtdiode (en: light emitting diode) LVT Losvalidierungsprfung (en: lot validation testing) MMIC monolithisch integrierte Mikrowellenschaltung (en: microwave monolithic integrated circuit) PAD Teilezulassungsdokument (e
17、n: parts approval document) PCB Teileschalttafel (en: parts control board) PCN Prozessnderungsbenachrichtigung (en: process change notice) PDA zulssiger Fehleranteil (en: percent defective allowable) PED kunststoffummanteltes Bauteil (en: plastic encapsulated device) PIND Partikel-Auswirkungs-Gerusc
18、h-Abfragung (en: particle impact noise detection) QBSD Vollquadrant-Detektor von zurckgestreuten Elektronen (en: full quadrant back scatter electron detector) QCI Qualittsentsprechungsinspektion (en: quality conformance inspection) RFD Abweichungsantrag (en: request for deviation) RH relative Luftfe
19、uchte (en: relative humidity) RoHs Einschrnkung des Gebrauchs bestimmter gefhrlicher Subtanzen (en: restriction of the use of certain hazardous substances) RVT Strahlungsverifikationsprfung (en: radiation verification testing) SCSB Raumfahrtkomponenten-Lenkungsausschuss (en: Space Components Steerin
20、g Board) SAM Ultraschallmikroskopie (en: scanning accoustic microscopy) SEM Rasterelektronenmikroskopie (en: scanning electron microscope) SMD oberflchenmontierbares Bauteil (en: surface mount device) TCI Technikkonformittsinspektion (en: technology conformance inspection) Tg Glassivationstemperatur
21、 (en: glassivation temperature) THB Temperatur-Feuchtigkeits-Einfluss (en: temperature humidity bias) Tj Verbindungstemperatur (en: junction temperature) T/C Temperaturwechselbeanspruchung (en: thermal cycling) DIN EN 16602-60-13:2015-11 6 Leerseite EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM
22、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 lutilisation de composants commerciaux sur tagre Raumfahrtproduktsicherung - Anforderungen fr die Nutzung von COTS-Kompo
23、nenten 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
24、 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
25、 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
26、, 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
27、 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 16602-60-13:2015 EEN 16602-60-13:2015 (E) 2 Table of content
28、s 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 3.2 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 co
29、mponents . 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 retinned parts 75 9 Pure tin lead finish risk analysis 83 Annex A (normative) Component control plan (CCP) - DRD . 84 Annex B (normative) Declar
30、ed components list (DCL) - DRD . 85 Annex C (normative) Internal Suppliers specification - DRD . 86 Annex D (normative) Parts approval document - DRD 88 Annex E (informative) EEE documents delivery per review 89 Annex F (normative) Justification document - DRD 90 Annex G (informative) Difference bet
31、ween the three classes . 93 Annex H (informative) Flow chart for construction analysis and destructive physical analysis . 94 DIN EN 16602-60-13:2015-11 EN 16602-60-13:2015 (E) 3 Bibliography . 98 Figures Figure 4-1: Evaluation tests flow chart for Class 1 components 21 Figure 4-2: Lot acceptance te
32、sts 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 Class 2 components 51 Figure 6-1: Lot acceptance test flow chart for Class 3 components 67 Figure 8-1: Evaluation flow chart for retinned part
33、s 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 class 2 programmes . 79 Figure 8-4: Lot acceptance flow chart for retinned parts class 2 programmes . 80 Figure 8-5: Evaluation flow chart f
34、or 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 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
35、 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 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 Cl
36、ass 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 Class 3 components 73 Table H-1 : Construction analysis and DPA 94 Table H-2 : Construction analysis sequence . 95 Table H-3 : Destructive
37、 physical analysis sequence . 97 DIN EN 16602-60-13:2015-11EN 16602-60-13:2015 (E) 4 European foreword This document (EN 16602-60-13:2015) has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-60-13:2015) originates from ECSS-
38、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 February 2016, and conflicting national standards shall be withdrawn at the latest by February 2016. Attention is drawn to the possibil
39、ity 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 Asso
40、ciation. 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 f
41、ollowing 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, Netherland
42、s, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. DIN EN 16602-60-13:2015-11 EN 16602-60-13:2015 (E) 5 Introduction This European Standard is based on and complementary to ECSS-Q-ST-60C (with upward revisions). This standard can only
43、 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 technical parameters that are on the system application level demonstrated to be unachievable with existing space components or only
44、achievable with qualitative and quantitative penalties. The standard requires that qualitative and quantitative penalties are specified, as applicable, as a minimum in terms of quantifiable parameters such as: functional capability, parts count, power dissipation, frequency of operation, data/signal
45、 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 unmodified text. The objective of the EEE component selection, control, procurement and use requirements is to ensure that EEE c
46、omponents 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 assuranc
47、e, 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
48、. 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 confid
49、ence, and DIN EN 16602-60-13:2015-11 EN 16602-60-13:2015 (E) 6 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,
