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EN 3783:2013

Current

Current

The latest, up-to-date edition.

Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties

Published date

21-08-2013

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Foreword
1 Scope and field of application
2 Normative references
3 Principle
4 Designation
5 Procedure
6 Test report

This standard describes the procedure for normalisation of fibre dominated mechanical properties. The procedure is valid for carbon, glass and aramid reinforced laminates.

Committee
ASD-STAN
DevelopmentNote
Supersedes PREN 3783. (09/2013)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
NF EN 3783 : 2015 Identical
NBN EN 3783 : 2013 Identical
NEN EN 3783 : 2013 Identical
NS EN 3783 : 2013 Identical
I.S. EN 3783:2013 Identical
PN EN 3783 : 2013 Identical
SN EN 3783 : 2013 Identical
UNI EN 3783 : 2014 Identical
UNE-EN 3783:2013 Identical
BS EN 3783:2013 Identical
DIN EN 3783:2013-12 Identical

93/706616 DC : 0 PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL
PREN 2833-1 : 200P2 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS
I.S. EN 2833-005:2013 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE
EN 2850:2017 Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction
BS EN 2850:2017 Aerospace series. Carbon fibre thermosetting resin - Unidirectional laminates. Compression test parallel to fibre direction
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
UNI EN 2833-005 : 2014 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE
EN 2833-005:2013 Aerospace series - Glass fibre thermosetting preimpregnates - Technical specification - Part 005: Glass fabric/phenolic resin preimpregnate
93/711194 DC : 0 PREN 2833-2 - TECHNICAL SPECIFICATION - GLASS FIBRE THERMOSETTING PREIMPREGNATES - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C
BS EN 2833-005:2013 Aerospace series. Glass fibre thermosetting preimpregnates. Technical specification Glass fabric/phenolic resin preimpregnate
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
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
I.S. EN 2850:2017 AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN - UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION

EN 2329:1993 Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of mass per unit area
EN 2557:1997 Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area

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