EN 2561:1995
Current
The latest, up-to-date edition.
Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates - Tensile test parallel to the fibre direction
20-09-1995
Foreword
1 Scope
2 Normative references
3 Definitions
4 Principle
5 Apparatus
6 Specimens
7 Procedure
8 Expression of results
9 Designation
10 Test report
Annex A (normative) Form, dimensions of specimen, test
fixture
This standard specifies the method of determination of the ultimate tensile strength, tensile modulus and, if required, the Poisson'ratio and elongation at failure in tension of carbon fibre reinforced plastics in the form of unidirectional laminates. This method is only applicable to specimens where the axis is parallel to the direction of the fibres.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2561. (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| UNE-EN 2561:1996 | Identical |
| NS EN 2561 : 1ED 1995 | Identical |
| NBN EN 2561 : 1996 | Identical |
| NEN EN 2561 : 1995 | Identical |
| UNI EN 2561 : 1995 | Identical |
| BS EN 2561:1995 | Identical |
| SNV DIN EN 2561 : 1995 | Identical |
| NF EN 2561 : 1996 | Identical |
| DIN EN 2561:1995-11 | Identical |
| PN EN 2561 : 1999 | Identical |
| I.S. EN 2561:1996 | Identical |
| NBN EN 2355 : 1993 | Identical |
| 17/30353428 DC : DRAFT JUNE 2017 | BS EN 17129 - CONTINUOUS-FIBRE-REINFORCED PLASTIC COMPOSITES - PULTRUDED UNIDIRECTIONAL RODS - DETERMINATION OF TENSILE PROPERTIES IN PARALLEL TO THE FIBRE DIRECTION |
| SAE AMS 3970/6 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2] |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| PREN 17129 : DRAFT 2017 | CONTINUOUS-FIBRE-REINFORCED PLASTIC COMPOSITES - PULTRUDED UNIDIRECTIONAL RODS - DETERMINATION OF TENSILE PROPERTIES IN PARALLEL TO THE FIBRE DIRECTION |
| EN 2489:1995 | Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| PREN 2565 : 200P2 | AEROSPACE SERIES - PREPARATION OF CARBON FIBRE REINFORCED RESIN PANELS FOR TEST PURPOSES |
| PREN 2823 : 200P2 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS |
| EN 2744:1992 | Aerospace series - Non metallic materials - Preferred test temperatures |
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