EN 16602-60-13:2023
(Main)Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components
Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components
2021-04-21: This EN is based on ECSS-Q-ST-60-13C Rev.1
Raumfahrtproduktsicherung - Kommerzielle, elektrische, elektronische und elektromechanische (EEE) Bauteile
The purpose of this NWIP is to update EN 16602-60-13(2015), equivalent to ECSS-Q-ST-60-13C “Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components”.
The objectives of this activity are:
1. To disposition all CRs and propose their implementation.
2. Pre-tailoring:
a. The C version of the ECSS-Q-ST-60-13 standard already provides three classes of EEE COTS components, in line with the ECSS-Q-ST-60C Rev.2, but the need for modification to the current type of Pre-Tailoring shall be discussed by the WG and the result reported to the TA for instructions.
b In case the WG believe there will be a need for modification to the current Pre-Tailoring, they will present their request to the TA and specific instructions will be provided.
3. To improve the general usability of the standard by defining requirement rationale where necessary, as specified in Annex B of the present document. The way this information will be published is still to be defined by the TA. The result shall be recorded in a separate document until further instruction by TA.
Justification:
Change Requests have been issued and reviewed by the discipline TAAR. The TA, based on the TAAR assessment, concluded that some of them are important enough and urgent and, as a consequence, required an update of the document.
All CRs recorded on this document shall then be reviewed and implemented by the Policy & Standards Working Group (PSWG) of ESCC that can be supported, if needed, by additional COTS experts that can be properly proposed by the PSWG and approved by the TA and the activities listed in clause 1 shall be carried out.
As identified by the Task Force on New Space Activities, the use of COTS in the current evolving equipment technology is becoming massive and the possibility to use EEE components coming from different business types (Automotive, Aeronautic, Railway, etc.) shall be taken into account .
In addition to the small technical and editorial modifications of Q-ST-60-13C requirements which have been proposed by the attached CRs, the additional following main technical topics have been identified as needed to be implemented:
- Enlargement of ECSS-Q-ST-60-13C Rev.1 to passive parts: enlarging the scope of the ECSS-Q-ST-60-13 current issue, by adding requirements about passive parts procurement (the scope of the current issue is limited to active parts).
- Automotive standard recognition: This new work item proposal aimed at defining the way to recognize automotive standards (AEC-Q) in EEE parts procurement process.
- Screening and re-tinning requirements modification: This new work item proposal aimed at reducing screening and re-tinning requirements in certain cases.
Assurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE) commerciaux
Zagotavljanje varnih proizvodov v vesoljski tehniki - Električne, elektronske in elektromehanske komercialne komponente (EEE)
Ta standard določa zahteve za izbiro, nadzor, nabavo in uporabo komercialnih električnih, elektronskih in elektromehanskih komponent (EEE) za vesoljske projekte.
Ta standard se uporablja za komercialne dele iz naslednjih skupin:
• čipi keramičnega kondenzatorja,
• čipi tantalskega kondenzatorja s trdnim elektrolitom,
• diskretni deli (tranzistorji, diode, optični sklopniki),
• varovalke,
• magnetni deli,
• mikrovezja,
• uporni čipi,
• termistorji.
Poleg tega se lahko za družine električnih, elektronskih in elektromehanskih komponent (EEE), ki jih ta standard ECSS ne obravnava, uporablja kot smernica za vsak primer posebej.
Zahteve tega dokumenta veljajo za vse vpletene strani na vseh ravneh integracije komercialnih 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
Relations
Standards Content (Sample)
SLOVENSKI STANDARD
01-september-2023
Zagotavljanje varnih proizvodov v vesoljski tehniki - Električne, elektronske in
elektromehanske komercialne komponente (EEE)
Space product assurance - Commercial electrical, electronic and electromechanical
(EEE) components
Raumfahrtproduktsicherung - Kommerzielle Elektrische, elektronische und
elektromechanische (EEE) Bauteile
Assurance produit des projets spatiaux - Composants électriques, électroniques et
électromécaniques (EEE) commerciaux
Ta slovenski standard je istoveten z: EN 16602-60-13:2023
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD EN 16602-60-13
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2023
ICS 49.140
Supersedes EN 16602-60-13:2015
English version
Space product assurance - Commercial electrical,
electronic and electromechanical (EEE) components
Assurance produit des projets spatiaux - Composants Raumfahrtproduktsicherung - Kommerzielle
électriques, électroniques et électromécaniques (EEE) Elektrische, elektronische und elektromechanische
commerciaux (EEE) Bauteile
This European Standard was approved by CEN on 30 January 2023.
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, France, Germany, Greece, Hungary, Iceland, Ireland, Italy,
Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Republic of North Macedonia, Romania, Serbia,
Slovakia, Slovenia, Spain, Sweden, Switzerland, Türkiye and United Kingdom.
CEN-CENELEC Management Centre:
Rue de la Science 23, B-1040 Brussels
© 2023 CEN/CENELEC All rights of exploitation in any form and by any means
Ref. No. EN 16602-60-13:2023 E
reserved worldwide for CEN national Members and for
CENELEC Members.
Table of contents
European Foreword . 5
Introduction . 6
1 Scope . 8
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
3.6 Convention for the Applicability Matrix . 15
4 Requirements for class 1 components . 16
5 Requirements for class 2 components . 28
6 Requirements for class 3 components . 39
7 Quality levels . 50
8 Evaluation, screening and LAT tests . 51
9 Pure tin lead finish – risk analysis . 93
Annex A (normative) Component control plan (CCP) - DRD . 94
Annex B (normative) Declared components list (DCL) - DRD . 95
Annex C (normative) Internal Supplier’s specification - DRD . 96
Annex D (normative) Parts approval document - DRD . 97
Annex E (informative) EEE documents delivery per review . 98
Annex F (normative) Justification document - DRD . 99
Annex G <> . 102
Annex H (informative) Flow chart for construction analysis . 103
Bibliography . 106
Figures
Figure 4-1: <> . 20
Figure 4-2: <> . 23
Figure 5-1: <> . 32
Figure 5-2: <> . 35
Figure 6-1: <> . 45
Figure 8-1: <> .51
Figure 8-2: <> .51
Figure 8-3: <> .51
Figure 8-4: <> .51
Figure 8-5: <> .51
Figure 8-6: <> .51
Tables
Table 4–1: <> . 20
Table 4–2: <> . 23
Table 4–3: <> . 23
Table 4-4: Documentation for Class 1 components . 27
Table 5–1: <> . 32
Table 5–2: <> . 34
Table 5–3: <> . 35
Table 5–4: Documentation for Class 2 components . 38
Table 6–1: <> .42
Table 6–2: <> .44
Table 6–3: <> . 45
Table 6–4: Documentation for Class 3 components . 48
Table 8–1: Procurement test table for ceramic capacitors chips . 54
Table 8–2: Procurement test table for solid electrolyte tantalum capacitors chips . 56
Table 8–3: Procurement test table for discrete parts (diodes, transistors, optocouplers)
..................................................................................................................58
Table 8–4: Procurement test table for fuses .60
Table 8–5: Procurement test table for magnetics.63
Table 8–6: Procurement test table for microcircuits . 66
Table 8–7: Procurement test table for resistor chips . 68
Table 8–8: Procurement test table for Thermistors . 71
Table 8–9: Legacy test files - Evaluation tests for Class 1 components - Active parts . 74
Table 8–10: Legacy test files - Screening tests for Class 1 components - Active parts 77
Table 8–11: Legacy test files - Lot acceptance tests for Class 1 components - Active
parts .79
Table 8–12: Legacy test files - Evaluation tests - Class 2 components - Active parts . 82
Table 8–13: Legacy test files - Screening tests - Class 2 components - Active parts . 85
Table 8–14: Legacy test files - Lot acceptance tests - Class 2 components – Active parts
..................................................................................................................87
Table 8–15: Legacy test files - LAT tests - Class 3 components - Active parts . 90
: <> . 103
: Construction analysis sequence . 104
European Foreword
This document (EN 16602-60-13:2023) has been prepared by Technical
Committee CEN-CENELEC/TC 5 “Space”, the secretariat of which is held by
DIN.
This standard (EN 16602-60-13:2023) originates from ECSS-Q-ST-60-13C Rev.1.
This document will supersede EN 16602-60-13:2015.
The main changes with respect to EN 16602-60-13:2015 are listed below:
• Implementation of Change Requests
• Definition of “traceability information (trace code)” updated”
• Alignment with updated version of ECSS-Q-ST-60
This document has been prepared under a standardization request 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).
Introduction
This standard is based on and complementary to ECSS-Q-ST-60C. It defines the
applicability and tailoring of the requirements of ECSS-Q-ST-60C for COTS EEE.
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 technical 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 terms 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 unmodified text.
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 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”.
In line with ECSS-Q-ST-60, 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 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.
Class 1 components are described in Clause 4
Class 2 components are described in Clause 5
Class 3 components are described in Clause 6
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:
component programme management,
component selection, evaluation and approval,
procurement,
handling and storage,
component quality assurance,
specific components, and
documentation.
The main tools which can be used to reach the objective are:
concurrent engineering,
standardization of component types,
characterization of components,
assessment of component manufacturers including declared competencies
and processes,
testing, screening, lot acceptance and periodic testing,
procurement specifications,
control and inspection,
control of nonconforming materials,
assessment and use of existing component data,
...
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