EN 2329:1993
Current
The latest, up-to-date edition.
Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of mass per unit area
03-03-1993
Cooperating organizations
National foreword
Foreword
1 Scope
2 Normative references
3 Definitions
4 Principle
5 Apparatus
6 Atmosphere for conditioning and testing
7 Sampling and specimens
8 Procedure
9 Calculation and expression of results
10 Test report
National annex NA (informative) Committees responsible
This standard specifies a method for determining the mass per unit area of a textile glass fibre preimpregnate, for aerospace use. This standard does not give any directives necessary to meet the health and safety requirements. It is the responsibility of the user of this standard to adopt appropriate health and safety precautions.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2329. (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NEN EN 2329 : 1993 | Identical |
| DIN EN 2329:1993-04 | Identical |
| PN EN 2329 : 1996 | Identical |
| SNV DIN EN 2329 : 1993 | Identical |
| BS EN 2329:1993 | Identical |
| UNE-EN 2329:1996 | Identical |
| NF EN 2329 : 1993 | Identical |
| NBN EN 2329 : 1993 | Identical |
| NS EN 2329 : 1ED 1993 | Identical |
| I.S. EN 2329:1993 | Identical |
| UNI EN 2329 : 1993 | Identical |
| UNE-EN 2329:1993 | Identical |
| 93/706616 DC : 0 | PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL |
| PREN 3783 : 200P1 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| BS EN 2331:1993 | Textile glass fibre preimpregnates. Test method for the determination of the resin and fibre content and mass of fibre per unit area |
| DIN EN 2331:1993-04 | AEROSPACE SERIES - TEXTILE GLASS FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN AND FIBRE CONTENT AND MASS OF FIBRE PER UNIT AREA |
| PREN 2833-1 : 200P2 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
| SAE AMS 3970/5 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 5: PURCHASING SPECIFICATION FOR COMPANION NON-STRUCTURAL GLASS FIBER FABRIC PREPREG |
| BS EN 3783:2013 | Aerospace series. Fibre composite materials. Normalisation of fibre dominated mechanical properties |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| I.S. EN 3783:2013 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| EN 2331:1993 | Aerospace series - Textile glass fibre preimpregnates - Test methods for the determination of the resin and fibre content and mass of fibre per unit area |
| EN 3783:2013 | Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties |
| 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] |
| UNI EN 3783 : 2014 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
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