EN 16602-60-13:2015
(Main)Space product assurance - Requirements for the use of COTS components
Space product assurance - Requirements for the use of COTS components
This standard defines the requirements for selection, control, procurement and usage of EEE commercial components for space projects.
This standard is applicable to commercial encapsulated active monolithic parts (integrated circuits and discrete):
• diodes
• microwave diodes
• integrated circuits
• microwave integrated circuits (MMIC)
• transistors
• microwave transistors
This standard is not applicable to the commercial parts from the following families:
• capacitors
• connectors
• crystals
• filters
• fuses
• heaters
• inductors
• microwave passive parts
• oscillators
• relays
• resistors
• switches
• thermistors
• transformers
• cables & wires
• hybrids
• surface acoustic waves (SAW)
• charge coupled devices (CCD)
• active pixel sensors (APS)
In addition, the following families of EEE components are not addressed by the present ECSS standard but it can be used as guideline and revisited on case/case basis:
• photodiodes
• light emitting diodes (LED)
• phototransistors
• opto-couplers
• laser diodes
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.
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
Annex G includes a diagram that summarizes the difference between these three classes for evaluation, screening and lot acceptance.
The requirements of this document are applicable to all parties involved at all levels in the integration of EEE commercial components into space segment hardware and launchers.
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”.
This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
Raumfahrtproduktsicherung - Anforderungen für die Nutzung von COTS-Komponenten
Assurance produit des projets spatiaux - Exigences pour l'utilisation de composants commerciaux sur étagère
Zagotavljanje varnih proizvodov v vesoljski tehniki - Zahteve za uporabo COST-komponent
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 vdelane aktivne monolitne dele (integrirana vezja in diskretne elemente): •diode •mikrovalovne diode •integrirana vezja •mikrovalovna integrirana vezja (MMIC) •tranzistorji •mikrovalovni tranzistorji Ta standard se ne uporablja za komercialne dele iz naslednjih družin: •kondenzatorji •priključki •kristali •filtri •varovalke •grelniki •induktorji •mikrovalovni pasivni deli •oscilatorji •releji •upori •stikala •termistorji •transformatorji •kabli in žice •hibridi •površinski zvočni valovi (SAW) •naprava za pretok električnega naboja (CCD) •senzorji za aktivne slikovne pike (APS) Naslednje družine električnih, elektronskih in elektromehanskih komponent tudi niso vključene v trenutni standard ECSS, vendar se standard lahko uporablja kot smernica in obravnava za vsak primer posebej: •fotodiode •svetleče diode (LED) •fototranzistorji •opto-sklopniki •laserske diode V skladu z ECSS-Q-ST-60 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. Dodatek G vključuje shemo, ki povzema razlike med temi tremi razredi za ovrednotenje, presejanje in sprejemljivost serije. Zahteve tega dokumenta veljajo za vse vpletene strani na vseh ravneh integracije komercialnih električnih, elektronskih in elektromehanskih komponent v vesoljski strojni opremi in lansirnikih. Za lažje prilagajanje in uvajanje zahtev v orodje za upravljanje zahtev ter za neposredno sledljivost do ECSS-Q-ST-60 so zahteve v tem standardu napisane na način ECSS EARM (Applicability Requirement Matrix), kot je določeno v dodatku A k standardu ECSS-S-ST-00 »ECSS system – Description, implementation and general requirements« (Sistem ECSS – Opis, izvajanje in splošne zahteve). Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Zagotavljanje varnih proizvodov v vesoljski tehniki - Zahteve za uporabo COST-komponentRaumfahrtproduktsicherung - Anforderungen für die Nutzung von COTS-KomponentenAssurance produit des projets spatiaux - Exigences pour l'utilisation de composants commerciaux sur étagèreSpace product assurance - Requirements for the use of COTS components49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16602-60-13:2015SIST EN 16602-60-13:2015en,fr,de01-oktober-2015SIST EN 16602-60-13:2015SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16602-60-13
August 2015 ICS 49.140
English version
Space product assurance - Requirements for the use of COTS components
Assurance produit des projets spatiaux - Exigences pour l'utilisation de composants commerciaux sur étagère
Raumfahrtproduktsicherung - Anforderungen für die Nutzung von COTS-Komponenten 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 16602-60-13:2015 E SIST EN 16602-60-13:2015
Figures Figure 4-1: Evaluation tests flow chart for Class 1 components . 21 Figure 4-2: Lot acceptance tests flow chart for Class 1 components . 28 Figure 5-1: Evaluation Tests flow charts for Class 2 components . 42 Figure 5-2: Lot acceptance tests flow chart for Class 2 components . 51 Figure 6-1: Lot acceptance test flow chart for Class 3 components . 67 Figure 8-1: Evaluation flow chart for retinned parts – class 1 programmes . 76 Figure 8-2: Lot acceptance flow chart for retinned parts – class 1 programmes . 77 Figure 8-3: Evaluation flow chart for retinned parts – class 2 programmes . 79 Figure 8-4: Lot acceptance fl
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