EN 16602-60-14:2020
(Main)Space product assurance - Relifing procedure - EEE components
Space product assurance - Relifing procedure - EEE components
This standard specifies the requirements, also known as "relifing requirements", for the planned, intentional storage, control, and removal from storage of electronic, electrical and electromechanical parts which are intended to be used for space applications.
This standard covers the relifing of all components as defined by ECSS-Q-ST-60 and ECSS-Q-ST-60-13.
The relifing process is a lot quality control activity. The inspections and tests defined do not constitute an up-screening or up-grading of components to a higher level of quality than procured to.
In line with ECSS-Q-ST-60, this standard differentiates between classes of components through different sets of standardization requirements.
The classes provide 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, 5 and 6
- Class 2 components are described in Clause 4, 5 and 6
- Class 3 components are described in Clause 4, 5 and 7
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 is applicable to all EEE parts covered by ECSS-Q-ST-60 and used in space programmes.
This standard is not applicable to dice.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Raumfahrtproduktsicherung - Wiederbelebungsprozeduren für EEE-Komponenten
Assurance produit des projets spatiaux - Procédure de remise en état - Composants EEE
La présente norme définit les exigences (également désignées « exigences de remise en
état ») relatives au stockage, à la manutention et au déstockage planifiés et volontaires
des composants électroniques, électriques et électromécaniques destinés aux
applications spatiales.
La présente norme couvre la remise en état de tous les composants tels que définis par
l’ECSS-Q-ST-60 et l’ECSS-Q-ST-60-13.
Le processus de remise en état relève de la maîtrise de la qualité. Les contrôles et essais
définis ne constituent pas une valorisation ou une mise à niveau des composants à un
seuil de qualité supérieur à celui pour lequel ils ont été fournis.
Conformément à l’ECSS-Q-ST-60, la présente norme différencie les classes de
composants au moyen de différents ensembles d’exigences de normalisation.
Les classes fournissent des niveaux de comparaison entre l’assurance et le risque.
L’assurance optimale et le risque minimal sont fournis par la classe 1, tandis que
l’assurance la plus faible et le risque le plus élevé relèvent de la classe 3. Les coûts
d’approvisionnement sont en général les plus élevés pour la classe 1 et les plus bas pour
la classe 3. Des mesures d’atténuation et autres mesures techniques peuvent faire baisser
les différences de coût total de possession entre les trois classes. Les objectifs, la définition
et les contraintes du projet déterminent la ou les classes de composants appropriée(s) à
utiliser dans le système et les sous-systèmes.
· Les composants de classe 1 sont décrits dans l’Article 4, l’Article 5 et l’Article 6.
· Les composants de classe 2 sont décrits dans l’Article 4, l’Article 5 et l’Article 6.
· Les composants de classe 3 sont décrits dans l’Article 4, l’Article 5 et l’Article 7.
Les exigences du présent document s’appliquent à l’ensemble des parties impliquées à
tous les niveaux de l’intégration des composants EEE dans le matériel spatial et les
lanceurs.
La présente norme s'applique à l'ensemble des composants EEE concernés par l'ECSS-QST-
60 et utilisés dans le cadre de programmes spatiaux.
Elle ne concerne pas les microplaquettes.
La présente norme peut être adaptée aux caractéristiques et contraintes spécifiques d’un
projet spatial, conformément à l’ECSS-S-ST-00.
Zagotavljanje varnih proizvodov v vesoljski tehniki - Postopek obnovitve uporabnosti - Komponente EEE
General Information
Relations
Standards Content (Sample)
SLOVENSKI STANDARD
01-november-2020
Nadomešča:
SIST EN 16602-60-14:2015
Zagotavljanje varnih proizvodov v vesoljski tehniki - Postopek obnovitve
uporabnosti - Komponente EEE
Space product assurance - Relifing procedure - EEE components
Raumfahrtproduktsicherung - Wiederbelebungsprozeduren für EEE-Komponenten
Assurance produit des projets spatiaux - Procédure de déstockage - Composants EEE
Ta slovenski standard je istoveten z: EN 16602-60-14:2020
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 16602-60-14
NORME EUROPÉENNE
EUROPÄISCHE NORM
September 2020
ICS 49.140
Supersedes EN 16602-60-14:2014
English version
Space product assurance - Relifing procedure - EEE
components
Assurance produit des projets spatiaux - Procédure de Raumfahrtproduktsicherung -
remise en état - Composants EEE Wiederbelebungsprozeduren für EEE-Komponenten
This European Standard was approved by CEN on 19 July 2020.
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, Turkey and United Kingdom.
CEN-CENELEC Management Centre:
Rue de la Science 23, B-1040 Brussels
© 2020 CEN/CENELEC All rights of exploitation in any form and by any means Ref. No. EN 16602-60-14:2020 E
reserved worldwide for CEN national Members and for
CENELEC Members.
Table of contents
European Foreword . 4
1 Scope . 5
2 Normative references . 6
3 Terms, definitions and abbreviated terms . 7
3.1 Terms from other standards . 7
3.2 Terms specific to the present standard . 7
3.3 Abbreviated terms. 10
3.4 Symbols . 11
3.5 Nomenclature . 11
4 Environmental parameters for handling and storage for Class 1 to Class 3
programmes . 13
4.1 General rules and requirements. 13
4.1.1 <> . 13
4.1.2 Procedures . 13
4.1.3 Storage area and storage zone . 13
4.1.4 Cleanliness . 13
4.1.5 ESD protection . 14
4.1.6 Packing – Packaging – Handling . 14
4.1.7 Quality assurance requirements for storage areas . 14
4.2 Storage conditions . 14
4.2.1 Air . 14
4.2.2 Temperature . 14
4.2.3 Relative humidity (RH) . 14
4.2.4 Container . 15
5 Timing parameters for Class 1 to Class 3 programmes . 16
6 Control parameters for Class 1 and Class 2 programmes . 18
6.1 Test requirements . 18
6.1.1 Requirements per EEE parts family: . 18
6.1.2 <> . 22
6.1.3 Electrical testing . 22
6.1.4 External visual inspection . 23
6.1.5 Seal test . 23
6.2 Nonconformance . 23
6.3 Relifing datecode . 23
6.4 Relifing report . 24
6.5 Certificate of Conformity . 24
7 Control parameters for Class 3 programmes . 25
7.1 Test requirements . 25
7.1.1 Requirements per EEE parts family . 25
7.1.2 Electrical testing . 27
7.1.3 External visual inspection . 27
7.2 Nonconformance . 27
7.3 Relifing datecode . 27
7.4 Relifing report . 28
7.5 Certificate of Conformity . 28
Annex A (normative) <>. 29
Annex B (informative) < . 30
Annex C (informative) Guidelines for a Relifing report . 31
Bibliography . 33
Figures
Figure C-1 : Example of a relifing traveller sheet . 32
Tables
Table 5-1: Timing parameters. 17
Table 6-1: Control parameters and detailed application of categories for Class 1 and
Class 2 programmes . 20
Table 7-1: Control parameters and detailed application of categories for Class 3
programmes . 26
European Foreword
This document (EN 16602-60-14:2020) has been prepared by Technical Committee
CEN-CENELEC/TC 5 “Space”, the secretariat of which is held by DIN.
This document (EN 16602-60-14:2020) originates from ECSS-Q-ST-60-14C Rev.1
Corrigendum 1.
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 March 2021,
and conflicting national standards shall be withdrawn at the latest by March
2021.
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 supersedes EN 16602-60-14:2014.
The main changes with respect to EN 16602-60-14:2014 are:
Creation of two relifing flows: one covering Class 1 and Class 2
components and the other covering Class 3 components
Harmonization with EN 16602-60:2015 (based on ECSS-Q-ST-60C Rev.2)
Introduction of the applicability of the relifing requirements to commercial
components
Change of timing requirements for relifing (from 7+3 to 7+4+4 years)
increasing the maximum elapsed time between date code and time of
mounting from 10 to 15 years
Transformation of normative Annex A "Relifing report - DRD" by into
informative Annex C "Guidelines for a Relifing report"
Deletion of informative Annex B "ESD".
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).
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, Serbia,
Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United
Kingdom.
Scope
This standard specifies the requirements, also known as “relifing requirements”,
for the planned, intentional storage, control, and removal from storage of
electronic, electrical and electromechanical parts which are intended to be used
for space applications.
This standard covers the relifing of all components as defined by ECSS-Q-ST-60
and ECSS-Q-ST-60-13.
The relifing process is a lot quality control activity. The inspections and tests
defined do not constitute an up-screening or up-grading of components to a
higher level of quality than procured to.
In line with ECSS-Q-ST-60, this standard differentiates between classes of
components through different sets of standardization requirements.
The classes provide 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, 5 and 6
Class 2 components are described in Clause 4, 5 and 6
Class 3 components are described in Clause 4, 5 and 7
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 is applicable to all EEE parts covered by ECSS-Q-ST-60 and used in
space programmes.
This standard is not applicable to dice.
This standard may be tailored for the specific characteristic and constrains of a
space project in conformance with ECSS-S-ST-00.
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 16602-10-09 ECSS-Q-ST-10-09 Space product assurance – Nonconformance control
system
EN 16602-60 ECSS-Q-ST-60 Space product assurance – Electrical, electronic and
electromechanical (EEE) components
EN 16602-60-13 ECSS-Q-ST-60-13 Space product assurance – Requirements for the use of
COTS components
EN 16602-70-01 ECSS-Q-ST-70-01 Space product assurance – Cleanliness and
contamination control
ESCC 24900 Minimum Requirements for Controlling Environmental
...
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