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

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.
This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) Bauteile

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

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. Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.

General Information

Status
Withdrawn
Publication Date
11-Aug-2015
Withdrawal Date
27-Jun-2023
Technical Committee
Drafting Committee
Current Stage

Relations

Buy Standard

Standard
EN 16602-60:2015
English language
98 pages
sale 10% off
Preview
sale 10% off
Preview
e-Library read for
1 day

Standards Content (Sample)


2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) BauteileAssurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)Space product assurance - Electrical, electronic and electromechanical (EEE) components49.140Vesoljski sistemi in operacijeSpace systems and operations49.060Aerospace electric equipment and systemsICS:Ta slovenski standard je istoveten z:EN 16602-60:2015SIST EN 16602-60:2015en,fr,de01-oktober-2015SIST EN 16602-60:2015SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16602-60
August 2015 ICS 49.140
English version
Space product assurance - Electrical, electronic and electromechanical (EEE) components
Assurance produit des projets spatiaux - Composants électriques, électroniques et électromécaniques (EEE)
Raumfahrtproduktsicherung - Elektrische, elektronische und elektromechanische (EEE) Bauteile 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 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, 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 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 16602-60:2015 E SIST EN 16602-60:2015
...

Questions, Comments and Discussion

Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.