EN 14101:2001
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
01-10-2014
24-10-2001
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-by means of laboratory tests in which specimens were either sprayed with salt water or periodically immersed and withdrawn; -by exposing specimens in sea coast or mild industrial environments; -by subjecting fabricated hardware to service conditions.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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