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EN 6035:2015

Current
Current

The latest, up-to-date edition.

Aerospace series - Fibre reinforced plastics - Test method - Determination of notched and unnotched tensile strength
Published date

11-25-2015

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 AMS 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES 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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