PREN 3783 : 200P1
Withdrawn
View Superseded by
AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES
Hardcopy , PDF
English
12-16-2023
1 Scope and field of application
2 References
3 Principle
4 Designation
5 Procedure
6 Test report
Describes the procedure for normalisation of fibre dominated mechanical properties.
| Committee |
C7
|
| DocumentType |
Draft
|
| Pages |
7
|
| ProductNote |
Superseded by EN 3783:2013
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| NFL 17 490 : *DUPLICATE RECORD* | Identical |
| NF EN 3783 : 2015 | Identical |
| DIN EN 3783:2013-12 | Identical |
| PREN 2833-3 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP 180 DEGREES C FOR CONTINUOUS USE UP TO 120 DEGREES C |
| PREN 2833-2 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT UP 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| PREN 2850 : 200P2 | AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION |
| PREN 2833-5 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 5: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| 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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