EN 2330:1993
Current
The latest, up-to-date edition.
Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of the content of volatile matter
03-03-1993
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
This standard specifies a method for determining the percentage of volatile matter in 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 2330. (11/2003)
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Current
|
Supersedes |
Standards | Relationship |
DIN EN 2330:1993-04 | Identical |
I.S. EN 2330:1993 | Identical |
SNV DIN EN 2330 : 1993 | Identical |
NS EN 2330 : 1ED 1993 | Identical |
NBN EN 2330 : 1993 | Identical |
UNI EN 2330 : 1993 | Identical |
NF EN 2330 : 1993 | Identical |
UNE-EN 2330:1996 | Identical |
PN EN 2330 : 1997 | Identical |
BS EN 2330:1993 | Identical |
NEN EN 2330 : 1993 | Identical |
UNE-EN 2330:1993 | 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 |
PREN 6085 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - EPOXY SURFACING FILMS |
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 |
PREN 6084 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - SURFACING FILMS - TECHNICAL SPECIFICATION - 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 |
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 |
DIN EN 2332:1993-04 | AEROSPACE SERIES - TEXTILE GLASS FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN FLOW |
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] |
BS EN 2332:1993 | Textile glass fibre preimpregnates. Test method for the determination of the resin flow |
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 2332:1993 | Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of the resin flow |
SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
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