EN 2557:1997
Current
The latest, up-to-date edition.
Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area
19-03-1997
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 AMS 3970/3 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES 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 AMS 3970/1 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES 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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