EN 16603-32-08:2016

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika - MaterialiRaumfahrttechnik - WerkstoffeIngénierie spatiale - MatériauxSpace engineering - Materials49.140Vesoljski sistemi in operacijeSpace systems and operationsICS:Ta slovenski standard je istoveten z:EN 16603-32-08:2016SIST EN 16603-32-08:2016en,fr,de01-november-2016SIST EN 16603-32-08:2016SLOVENSKI
STANDARDSIST EN 14607-8:20051DGRPHãþD

EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-32-08
August 2016 ICS 49.140 Supersedes EN 14607-8:2004
English version
Space engineering - Materials
Ingénierie spatiale - Matériaux
Raumfahrttechnik - Werkstoffe This European Standard was approved by CEN on 22 May 2016.
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 © 2016 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 16603-32-08:2016 E SIST EN 16603-32-08:2016

This standard specifies requirements for the establishment of the mechanical and physical properties of the materials to be used for space applications, and the verification of these requirements.
Verification includes destructive and non-destructive test methods. Quality assurance requirements for materials (e.g. procurement and control) are covered by ECSS-Q-ST-70. This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00. SIST EN 16603-32-08:2016

EN reference Reference in text Title EN 16601-00-01 ECSS-S-ST-00-01
ECSS system - Glossary of terms EN 16603-32 ECSS-E-ST-32 Space engineering -
Structural EN 16602-70 ECSS-Q-ST-70 Space product assurance - Materials, mechanical parts and processes EN 16602-70-37 ECSS-Q-ST-70-37 Space product assurance - Determination of the susceptibility of metals to stress-corrosion cracking EN 16602-70-71 ECSS-Q-ST-70-71 Space product assurance - Material, processes and their data selection
EN 4179:2005 Aerospace series - Qualification and approval of personnel for non-destructive testing SIST EN 16603-32-08:2016

1. A-basis design allowable (A-value) 2. B-basis design allowable (B-value) 3. corrosion 3.2 Terms specific to the present standard 3.2.1 composite sandwich construction panels composed of a lightweight core material, such as honeycomb, foamed plastic, and so forth, to which two relatively thin, dense, high-strength or high stiffness faces or skins are adhered 3.2.2 material design allowable material property that has been determined from test data on a probability basis and has been chosen to assure a high degree of confidence in the integrity of the completed structure 3.2.3 micro-yield applied force to produce a residual strain of 1 × 10-6 mm/m along the tensile or compression loading direction 3.2.4 polymer high molecular weight organic compound, natural or synthetic, with a structure that can be represented by a repeated small unit, the mer NOTE
E.g. polyethylene, rubber, and cellulose. SIST EN 16603-32-08:2016

Meaning ASTM
American Society for Testing Materials CFRP
carbon fibre reinforced plastic CMC
ceramic matrix composites CME
coefficient of moisture expansion CTE
coefficient of thermal expansion DRD
document requirements definition EB
electron beam EN
European Standard Kic
plane strain critical stress intensity factor Kiscc
plane strain critical stress intensity factor for a specific environment LEO
low Earth orbit MIG
metal inert gas MMC
metal matrix composite NDE
non-destructive evaluation NDI
non-destructive inspection NDT
non-destructive test PTFE
polytetrafluoroethylene SCC
stress-corrosion cracking STS
space transportation system TIG
tungsten inert gas UD
uni-directional UV
ultra violet 3.4 Nomenclature The following nomenclature applies throughout this document: a. The word “shall” is used in this standard to express requirements. All the requirements are expressed with the word “shall”. b. The word “should” is used in this standard to express recommendations. All the recommendations are expressed with the word “should”. NOTE It is expected that, during tailoring, recommendations in this document are either converted into requirements or tailored out. c. The words “may” and “need not” are used in this standard to express positive and negative permissions, respectively. All the positive SIST EN 16603-32-08:2016
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