EN 16602-60-13:2023

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,
...