EN 2557:1997
Current
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The latest, up-to-date edition.
Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area
Published date
19-03-1997
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Foreword
1 Scope
2 Normative references
3 Principle
4 Apparatus
5 Specimens
6 Procedure
7 Expression of results
8 Health and safety requirements
9 Test report
This standard specifies a method for determining the mass per unit area of carbon fibre preimpregnates for aerospace applications.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2557. (10/2002)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| BS EN 2557:1997 | Identical |
| NBN EN 2257 : 1997 | Identical |
| PN EN 2557 : 2000 | Identical |
| NS EN 2557 : 1ED 1997 | Identical |
| NF EN 2557 : 1997 | Identical |
| UNI EN 2557 : 1998 | Identical |
| SNV DIN EN 2557 : 1997 | Identical |
| UNE-EN 2557:1997 | Identical |
| NEN EN 2557 : 1997 | Identical |
| DIN EN 2557:1997-05 | Identical |
| I.S. EN 2557:1997 | Identical |
| NBN EN 2557 : 1997 | Identical |
| PREN 3783 : 200P1 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| BS 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] |
| SAE AMS3970/3A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Carbon Prepreg |
| 00/702576 DC : 0 | PREN 4107 - AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - FOAMING ADHESIVES - TECHNICAL SPECIFICATION |
| I.S. EN 3783:2013 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| 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 |
| SAE AMS 3970/4 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 4: PURCHASING SPECIFICATION FOR FILM ADHESIVE |
| UNI EN 3783 : 2014 | AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES |
| EN 2743:2001 | Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials |
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