EN 16602-40-12:2014
(Main)Space product assurance - Fault tree analysis - Adoption notice ECSS/IEC 61025
Space product assurance - Fault tree analysis - Adoption notice ECSS/IEC 61025
This Standard defines requirements for the performance of Fault Tree Analysis (FTA) on space projects and incorporates the IEC 61025 standard into the ECSS system.
With effect from the date of approval, this Standard announces the adoption of the external document on a restricted basis for use in the European Cooperation for Space Standardization (ECSS) system.
This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.
Raumfahrtproduktsicherung - Fehlerbaumanalyse - Adoption notice ECSS/IEC 61025
Assurance produit des projets spatiaux - Analyse par arbre de panne - Notice d'adoption de la norme ECSS/CEI 61025
Zagotavljanje varnih proizvodov v vesoljski tehniki - Analiza drevesa okvar - Obvestilo o prevzemu (Adoption Notice) ECSS/IEC 61025
Ta standard določa zahteve za delovanje analize drevesa okvar (FTA) za vesoljske projekte in standard IEC 61025 vključuje v sistem ECSS.
Ta standard napoveduje sprejetje zunanjega dokumenta na omejeni podlagi za uporabo v sistemu evropskega sodelovanja za standardizacijo na področju vesolja (ECSS) z veljavnostjo od datuma odobritve.
Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.
General Information
- Status
- Published
- Publication Date
- 23-Sep-2014
- Withdrawal Date
- 30-Mar-2015
- Technical Committee
- CEN/CLC/TC 5 - Space
- Drafting Committee
- CEN/CLC/TC 5 - Space
- Current Stage
- 9060 - Closure of 2 Year Review Enquiry - Review Enquiry
- Start Date
- 03-Mar-2020
- Completion Date
- 03-Mar-2020
Relations
- Effective Date
- 28-Jan-2026
Overview
EN 16602-40-12:2014 is a European Standard focusing on space product assurance through Fault Tree Analysis (FTA). This standard integrates the internationally recognized IEC 61025 methodology into the European Cooperation for Space Standardization (ECSS) system. Its primary purpose is to define the requirements for conducting FTA on space projects, ensuring the analysis aligns with the specific demands and constraints of space systems.
FTA is a systematic, deductive failure analysis technique used to identify and evaluate the causes of system failures. By adopting IEC 61025 within the ECSS framework, this standard establishes a consistent approach to analyze potential faults that could impact spacecraft dependability and safety.
Key Topics
Fault Tree Analysis (FTA) Requirements: EN 16602-40-12:2014 specifies how to perform FTA on space-related projects, emphasizing its application for:
- Catastrophic, critical, or major undesirable events
- Failure mode support analysis
- Accident investigations
Adoption of IEC 61025 Principles: The standard adopts IEC 61025 fully, providing guidelines for:
- Preparation and execution of FTA
- Use of event symbols and fault logic structure
- Identification of failure assumptions and modes
Tailoring Flexibility: As stated in the standard, FTA procedures may be tailored following ECSS-S-ST-00, adapting them to the particular characteristics and constraints of each space project without compromising methodological integrity.
Supplier and Customer Collaboration: The supplier must seek customer agreement on FTA content and allow for customer reviews, ensuring transparency and alignment on analysis depth.
Software Utilization: When employing software tools to conduct FTA, any computer program used must:
- Support the necessary FTA functionalities
- Comply with project-specific requirements for data exchange and tool interoperability
- Note that the standard does not endorse specific proprietary software.
Applications
EN 16602-40-12:2014 is essential for organizations involved in the design, development, and assessment of space systems aiming to guarantee product safety and dependability. Its practical applications include:
Risk Assessment in Space Missions: Identifying root causes of system failures before launch to mitigate risks and increase mission success probability.
Failure Investigation: Serving as a structured approach to analyze accidents or anomalies during spacecraft operation, enabling informed corrective actions.
Requirement Verification: Ensures that safety and reliability goals related to critical failures are analyzed comprehensively and systematically.
Support for Safety Standards Compliance: Facilitates conformity with broader space product assurance standards within the ECSS framework.
By integrating FTA into the early stages of system engineering, project teams can preemptively address potential failure modes, reducing costly design errors and enhancing operational safety.
Related Standards
IEC 61025 – The foundational international standard for Fault Tree Analysis methodology adopted by EN 16602-40-12.
ECSS-Q-ST-30 – Space product assurance dependability standard that complements FTA requirements by defining dependability objectives and frameworks.
ECSS-Q-ST-40 – Space product assurance safety standard offering additional guidance on ensuring safety compliance.
ECSS-S-ST-00 – General system tailoring standard allowing the adaptation of fault analysis techniques like FTA to specific space project needs.
NUREG 0492 – Fault Tree Handbook by the U.S. Nuclear Regulatory Commission, a recommended supplementary resource for comprehensive fault tree practices.
Keywords: EN 16602-40-12:2014, Fault Tree Analysis, FTA, IEC 61025, ECSS, space product assurance, space mission reliability, fault tree methodology, fault analysis, space safety standards, aerospace fault tree analysis, ECSS standards, space systems dependability, fault tree software tools.
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Frequently Asked Questions
EN 16602-40-12:2014 is a standard published by the European Committee for Standardization (CEN). Its full title is "Space product assurance - Fault tree analysis - Adoption notice ECSS/IEC 61025". This standard covers: This Standard defines requirements for the performance of Fault Tree Analysis (FTA) on space projects and incorporates the IEC 61025 standard into the ECSS system. With effect from the date of approval, this Standard announces the adoption of the external document on a restricted basis for use in the European Cooperation for Space Standardization (ECSS) system. This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.
This Standard defines requirements for the performance of Fault Tree Analysis (FTA) on space projects and incorporates the IEC 61025 standard into the ECSS system. With effect from the date of approval, this Standard announces the adoption of the external document on a restricted basis for use in the European Cooperation for Space Standardization (ECSS) system. This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.
EN 16602-40-12:2014 is classified under the following ICS (International Classification for Standards) categories: 49.140 - Space systems and operations. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 16602-40-12:2014 has the following relationships with other standards: It is inter standard links to EN 80:2001. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 16602-40-12:2014 is associated with the following European legislation: Standardization Mandates: M/496. When a standard is cited in the Official Journal of the European Union, products manufactured in conformity with it benefit from a presumption of conformity with the essential requirements of the corresponding EU directive or regulation.
EN 16602-40-12:2014 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
SLOVENSKI STANDARD
01-januar-2015
Zagotavljanje varnih proizvodov v vesoljski tehniki - Analiza drevesa okvar -
Obvestilo o prevzemu (Adoption Notice) ECSS/IEC 61025
Space product assurance - Fault tree analysis - Adoption notice ECSS/IEC 61025
Raumfahrtproduktsicherung - Fehlerbaumanalyse - Adoption notice ECSS/IEC 61025
Assurance produit des projets spatiaux - Analyse par arbre de panne - Notice d'adoption
de la norme ECSS/CEI 61025
Ta slovenski standard je istoveten z: EN 16602-40-12:2014
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 16602-40-12
NORME EUROPÉENNE
EUROPÄISCHE NORM
September 2014
ICS 49.140
English version
Space product assurance - Fault tree analysis - Adoption notice
ECSS/IEC 61025
Assurance produit des projets spatiaux - Analyse par arbre Raumfahrtproduktsicherung - Fehlerbaumanalyse -
de panne - Notice d'adoption de la norme ECSS/CEI 61025 Adoption notice ECSS/IEC 61025
This European Standard was approved by CEN on 13 March 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
© 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved Ref. No. EN 16602-40-12:2014 E
worldwide for CEN national Members and for CENELEC
Members.
Table of contents
Foreword . 3
1 Scope . 4
2 Normative references . 5
3 Terms, definitions and abbreviated terms . 6
3.1 Terms defined in other standards . 6
3.2 Abbreviated terms. 6
4 Principles . 7
5 Requirements . 8
5.1 ECSS usage restriction . 8
5.1.1 Applicability . 8
5.1.2 Procedure . 8
5.1.3 Software tools supporting FTA . 9
Bibliography . 10
Foreword
This document (EN 16602-40-12:2014) has been prepared by Technical
Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN.
This standard (EN 16602-40-12:2014) originates from ECSS-Q-ST-40-12C.
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
2015, and conflicting national standards shall be withdrawn at the latest by
March 2015.
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 has been prepared under a mandate 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 nationa
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