SN EN 14101 : 2001
Current
The latest, up-to-date edition.
SPACE PRODUCT ASSURANCE - MATERIAL SELECTION FOR CONTROLLING STRESS-CORROSION CRACKING
12-01-2013
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
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. Intends to provide general criteria to be used in designing for resistance to stress-corrosion cracking.
DocumentType |
Standard
|
PublisherName |
Swiss Standards
|
Status |
Current
|
Standards | Relationship |
BS EN 14101:2001 | Identical |
UNI EN 14101 : 2002 | Identical |
EN 14101:2001 | Identical |
I.S. EN 14101:2002 | Identical |
UNE-EN 14101:2002 | Identical |
DIN EN 14101:2002-10 | Identical |
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