EN 6035:2015
Current
The latest, up-to-date edition.
Aerospace series - Fibre reinforced plastics - Test method - Determination of notched and unnotched tensile strength
25-11-2015
European foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test specimen
8 Procedure
9 Presentation of the results
10 Test report
This standard defines a method to be used to determine the tensile strength of notched and unnotched fibre reinforced plastics.It is applicable to composite laminates with unidirectional plies or woven fabrics reinforcement.This standard does not give any direction necessary to meet health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 6035. (12/2015)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NS EN 6035 : 2015 | Identical |
| SN EN 6035:2016 | Identical |
| NF EN 6035:2016 | Identical |
| NBN EN 6035 : 2015 | Identical |
| I.S. EN 6035:2015 | Identical |
| DIN EN 6035:2016-02 | Identical |
| UNI EN 6035 : 2016 | Identical |
| NEN EN 6035 : 2015 | Identical |
| PN EN 6035 : 2016 | Identical |
| BS EN 6035:2015 | Identical |
| UNE-EN 6035:2015 | Identical |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| 95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
| 95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
| 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] |
| PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| EN 2489:1995 | Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids |
| 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 2743:2001 | Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials |
| EN 2374:1991 | Aerospace series - Glass fibre reinforced mouldings and sandwich composites - Production of test panels |
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