EN 6038:2015
Current
The latest, up-to-date edition.
Aerospace series - Fibre reinforced plastics - Test method - Determination of the compression strength after impact
25-11-2015
European foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test specimen
8 Procedure
9 Presentation of the results
10 Test report
This European Standard defines a method to be used to measure the low speed impact resistance characteristics of fibre reinforced plastics.It is applicable to composite laminates with unidirectional plies or woven fabric reinforcement.This standard does not give any direction necessary to meet health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.
Committee |
ASD-STAN
|
DevelopmentNote |
Supersedes PREN 6038. (12/2015)
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Current
|
Supersedes |
Standards | Relationship |
UNI EN 6038 : 2016 | Identical |
SN EN 6038 : 2016 | Identical |
NF EN 6038 : 2017 | Identical |
NEN EN 6038 : 2015 | Identical |
NS EN 6038 : 2015 | Identical |
NBN EN 6038 : 2015 | Identical |
I.S. EN 6038:2015 | Identical |
BS EN 6038:2015 | Identical |
DIN EN 6038:2016-02 | Identical |
PN EN 6038 : 2016 | Identical |
UNE-EN 6038:2015 | Identical |
SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
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] |
PREN 2760 : 200P1 | AEROSPACE SERIES - STEEL FE-PL78 - 1760 <= R[M] <= 2000 MPA - BAR - D[E] <= 75 MM |
PREN 2565 : 200P2 | AEROSPACE SERIES - PREPARATION OF CARBON FIBRE REINFORCED RESIN PANELS FOR TEST PURPOSES |
EN 2743:2001 | Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials |
EN 2374:1991 | Aerospace series - Glass fibre reinforced mouldings and sandwich composites - Production of test panels |
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