Space engineering - Mechanical - Part 8: Materials

EN 14607 Part 8 of Space engineering - Mechanical defines the mechanical engineering requirements for materials.
This document also encompasses the effects of the natural and induced environments to which materials used for space applications can be subjected.
This document defines requirements for the establishment of the required mechanical and physical properties of the materials including the effects of the environmental conditions, material selection, procurement, production and verification. Verification includes destructive and non­destructive test methods. Material procurement and control is closely related to required quality assurance procedures and detailed references to EN 13291-3 are made.
When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project.
NOTE   Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements.

Raumfahrttechnik - Mechanik - Teil 8: Werkstoffe

Ingénierie spatiale - Mécanique - Partie 8: Matériaux

Vesoljska tehnika – Mehanika - 8. del: Materiali

General Information

Status
Withdrawn
Publication Date
03-Aug-2004
Withdrawal Date
23-Aug-2016
Technical Committee
Drafting Committee
Current Stage
9960 - Withdrawal effective - Withdrawal
Completion Date
24-Aug-2016

Relations

Effective Date
31-Aug-2016

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EN 14607-8:2005
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Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika – Mehanika - 8. del: MaterialiRaumfahrttechnik - Mechanik - Teil 8: WerkstoffeIngénierie spatiale - Mécanique - Partie 8: MatériauxSpace engineering - Mechanical - Part 8: Materials49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 14607-8:2004SIST EN 14607-8:2005en01-januar-2005SIST EN 14607-8:2005SLOVENSKI
STANDARD



SIST EN 14607-8:2005



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 14607-8August 2004ICS 49.140English versionSpace engineering - Mechanical - Part 8: MaterialsIngénierie spatiale - Mécanique - Partie 8: MatériauxRaumfahrttechnik - Mechanik - Teil 8: WerkstoffeThis European Standard was approved by CEN on 27 June 2003.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the Central Secretariat or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2004 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 14607-8:2004: ESIST EN 14607-8:2005



EN 14607-8:2004 (E) 2 Contents page Foreword.4 1 Scope.5 2 Normative references.5 3 Terms and definitions and abbreviated terms.5 3.1 Terms and definitions.5 3.2 Abbreviated terms.6 4 Requirements.7 4.1 General.7 4.1.1 Overview.7 4.1.2 Applicability.7 4.1.3 Controlling documentation.7 4.2 Mission.7 4.3 Functionality.7 4.3.1 Strength.7 4.3.2 Elastic modulus.7 4.3.3 Fatigue.8 4.3.4 Fracture toughness.8 4.3.5 Creep.8 4.3.6 Micro-yielding.8 4.3.7 Coefficient of thermal ex
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