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EN 14101:2001

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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Space product assurance - Material selection for controlling stress-corrosion cracking

Superseded date

01-10-2014

Superseded by

EN 16602-70-36:2014

Published date

24-10-2001

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Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
   3.1 Terms and definitions
   3.2 Abbreviated terms
4 Stress-corrosion
   4.1 Definition
        4.1.1 General
        4.1.2 Exclusions
   4.2 Grain orientation
   4.3 Stress considerations
   4.4 Susceptibility of engineering alloys
        4.4.1 Aluminium
        4.4.2 Steel
        4.4.3 Nickel
        4.4.4 Copper
5 Evaluation of metal alloys
6 Materials selection criteria
   6.1 High SCC resistance alloys
        6.1.1 General
        6.1.2 Thin materials
        6.1.3 Coated and plated materials
        6.1.4 Surface treated materials
   6.2 Moderate SCC resistance alloys
   6.3 Low SCC resistance alloys
   6.4 Unlisted materials
Annex A (normative) Stress-corrosion evaluation form
   A.1 Directions for completion
   A.2 Stress-corrosion evaluation form
Bibliography

This European Standard sets forth the criteria to be used in the selection of materials for spacecraft and associated equipment and facilities so that failure resulting from stress-corrosion is prevented.Three categories of materials are listed in Tables 1, 2 and 3 of this Standard. They represent metal alloys with a high, moderate and low resistance to stress-corrosion cracking. The stress-corrosion susceptibility of alloys included in this Standard was determined at ambient temperature -by means of laboratory tests in which specimens were either sprayed with salt water or periodically immersed and withdrawn; -by exposing specimens in sea coast or mild industrial environments; -by subjecting fabricated hardware to service conditions. Use of the criteria established herein should, therefore, be limited to designs for service involving similar exposure conditions.Weldments present a special problem in designing for resistance to stress-corrosion cracking. In addition to the susceptibility of the parent metals, it is also necessary to consider the filler metal and the microstructural effects of heat introduced by the welding operations and subsequent heat treatments. Because of the additional variables that shall be considered, susceptibility data are not as extensive for weldments as for alloys in mill form. Design criteria for weldments in this Standard are limited to aluminium alloys, selected stainless steels in the 300 series and other specific alloys listed in Table 1.This Standard is intended to provide general criteria to be used in designing for resistance to stress-corrosion cracking. Specific test data and other detailed information are not included.

Committee
CEN/BT
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Superseded
SupersededBy

Standards Relationship
I.S. EN 14101:2002 Identical
NEN EN 14101 : 2001 Identical
SN EN 14101 : 2001 Identical
NF EN 14101 : 2002 Identical
NS EN 14101 : 1ED 2002 Identical
UNI EN 14101 : 2002 Identical
UNE-EN 14101:2002 Identical
PN EN 14101 : 2002 Identical
BS EN 14101:2001 Identical
NBN EN 14101 : 2002 Identical
DIN EN 14101:2002-10 Identical

I.S. EN 13291-3:2004 SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 3: MATERIALS, MECHANICAL PARTS AND PROCESSES
BS EN 13291-3:2003 Space products assurance. General requirements Materials, mechanical parts and processes
EN 13291-3:2003 Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes
I.S. EN 14165:2004 SPACE ENGINEERING STANDARDS - FRACTURE CONTROL
BS EN 14607-5-1:2004 Space engineering. Mechanical Liquid and electric propulsion for spacecraft
DIN EN 13291-3:2005-03 SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 3: MATERIALS, MECHANICAL PARTS AND PROCESSES
I.S. EN 14607-5-1:2004 SPACE ENGINEERING - MECHANICAL - PART 5-1: LIQUID AND ELECTRIC PROPULSION FOR SPACECRAFT
03/301397 DC : DRAFT JAN 2003 EN 14607-5-1 - SPACE ENGINEERING - MECHANICAL - PART 5-1: LIQUID AND ELECTRIC PROPULSION FOR SPACECRAFT
03/311008 DC : DRAFT JUNE 2003 EN 14165 - SPACE ENGINEERING STANDARDS - FRACTURE CONTROL
BS EN 14165:2004 Space engineering standards. Fracture control
EN 14607-5-1:2004 Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft
EN 14165:2004 Space engineering standards - Fracture control
DIN EN 14165:2005-02 SPACE ENGINEERING STANDARDS - FRACTURE CONTROL

EN 13701:2001 Space systems - Glossary of terms
MIL-H-6088 Revision G:1991 HEAT TREATMENT OF ALUMINIUM ALLOYS
ANSI H35.1 : 2006 ALLOY AND TEMPER DESIGNATION SYSTEMS FOR ALUMINUM

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