EN 2377:1989
Current
The latest, up-to-date edition.
Aerospace series - Glass fibre reinforced plastics - Test method - Determination of apparent interlaminar shear strength
15-01-1989
Brief history
1 Scope and field of application
2 References
3 Definition
4 Principle of the method
5 Test specimens
6 Apparatus
7 Conditioning
8 Procedure
9 Test results
10 Calculation and expression of results
11 Test report
Annex A - Determination of the estimated value of
standard deviation
This standard defines a method for the determination of the apparent interlaminar shear strength by delamination of textile glass fibre reinforced plastics produced in sheet form for aerospace use.
Committee |
ASD-STAN
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Current
|
Standards | Relationship |
UNE-EN 2377:1993 | Identical |
DIN EN 2377:1989-10 | Identical |
BS EN 2377:1989 | Identical |
I.S. EN 2377:1992 | Identical |
UNI EN 2377 : 1989 | Identical |
NS EN 2377 : 1ED 1989 | Identical |
NEN EN 2377 : 1989 | Identical |
PN EN 2377 : 1994 | Identical |
NF EN 2377 : 1989 | Identical |
NBN EN 2377 : 1993 | Identical |
SNV DIN EN 2377 : 1989 | 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 2833-3 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP 180 DEGREES C FOR CONTINUOUS USE UP TO 120 DEGREES C |
PREN 2833-2 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT UP 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
I.S. EN 2833-005:2013 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
UNI EN 2833-005 : 2014 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
PREN 2833-5 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 5: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
XP PREN 2833-2 : 1995 XP | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT UPTO 125 DEGREES C FOR CONTINUOUS USE UPTO 80 DEGREES C |
EN 2833-005:2013 | Aerospace series - Glass fibre thermosetting preimpregnates - Technical specification - Part 005: Glass fabric/phenolic resin preimpregnate |
BS EN 2833-005:2013 | Aerospace series. Glass fibre thermosetting preimpregnates. Technical specification Glass fabric/phenolic resin preimpregnate |
95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
EN 62 : 1977 | GLASS REINFORCED PLASTICS - STANDARD ATMOSPHERES FOR CONDITIONING & TESTING |
EN 2374:1991 | Aerospace series - Glass fibre reinforced mouldings and sandwich composites - Production of test panels |
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