Space product assurance - Electrical, electronic and electromechanical (EEE) components

The Scope of the Standard remains unchanged.
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.

Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) Bauteile

Assurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)

La présente norme définit les exigences relatives à la sélection, au contrôle à l'approvisionnement et à l'utilisation des composants EEE dans le cadre des projets spatiaux.
La présente norme distingue trois classes de composants au moyen de trois ensembles différents d'exigences de normalisation (articles) à satisfaire.
Ces trois classes prévoient trois niveaux de compromis entre assurance et risque. L'assurance la plus élevée et le risque le plus bas sont fournis par la classe 1, et l'assurance la plus basse et le risque le plus élevé par la classe 3. Les coûts d'approvisionnement sont généralement les plus élevés pour la classe 1 et les plus bas pour la classe 3. La réduction et autres mesures d'ingénierie peuvent réduire les différences de coût global de possession entre les trois classes. Les objectifs, la définition et les contraintes du projet déterminent quelles classes de composants sont adaptées à une utilisation dans le système et les sous-systèmes.
a. Les composants de classe 1 sont décrits à l'Article 4.
b. Les composants de classe 2 sont décrits à l'Article 5.
c. Les composants de classe 3 sont décrits à l'Article 6.
Les exigences du présent document s'appliquent à toutes les parties impliquées à tous les niveaux de l'intégration des composants EEE dans le matériel de segment spatial et les lanceurs.
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 - 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.

General Information

Status
Published
Publication Date
27-Jun-2023
Technical Committee
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
28-Jun-2023
Due Date
23-Aug-2023
Completion Date
28-Jun-2023

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Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 16602-60:2023
01-september-2023
Nadomešča:
SIST EN 16602-60:2015
Zagotavljanje varnih proizvodov v vesoljski tehniki - Električne, elektronske in
elektromehanske komponente
Space product assurance - Electrical, electronic and electromechanical (EEE)
components
Space product assurance - Electrical, electronic and electromechanical (EEE)
components
Assurance produit des projets spatiaux - Composants électriques, électroniques et
électromécaniques (EEE)
Ta slovenski standard je istoveten z: EN 16602-60:2023
ICS:
49.060 Letalska in vesoljska Aerospace electric
električna oprema in sistemi equipment and systems
49.140 Vesoljski sistemi in operacije Space systems and
operations
SIST EN 16602-60:2023 en,fr,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 16602-60:2023

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SIST EN 16602-60:2023


EUROPEAN STANDARD EN 16602-60

NORME EUROPÉENNE

EUROPÄISCHE NORM
June 2023
ICS 49.140
Supersedes EN 16602-60:2015
English version

Space product assurance - Electrical, electronic and
electromechanical (EEE) components
Assurance produit des projets spatiaux - Composants Raumfahrtproduktsicherung - Elektrische,
électriques, électroniques et électromécaniques (EEE) elektronische und elektromechanische (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 16602-60:2023 E
reserved worldwide for CEN national Members and for
CENELEC Members.

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SIST EN 16602-60:2023
EN 16602-60:2023 (E)
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
4.1.6 EQM components .
...

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