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PREN 2850 : 200P2

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by
withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION
Available format(s)

Hardcopy , PDF

Withdrawn date

11-12-2023

Language(s)

English

Publisher

Aerospace & Defence Industries Association of Europe

1 Scope
2 Normative references
3 Principle of the method
4 Definitions
5 Designation
6 Test pieces
7 Apparatus
8 Conditioning
9 Procedure
10 Calculation of results
11 Validity
12 Test report
Normative annex A
Normative annex B
Informative annex C

Defines a method for the determination of stress at failure and Young's modulus in compression of carbon thermosetting resin unidirectional laminates.

Committee
C7
DocumentType
Draft
Pages
14
ProductNote
Superseded by EN 2850:2017
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Withdrawn
SupersededBy

Standards Relationship
DIN EN 2850:1998-04 (Draft) Identical

PREN 6044-2 : 200P1 AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - QUALIFICATION PROGRAMM/BATCH RELEASE TESTING - UNIDIRECTIONAL TAPE 180 DEGREE C CURING CLASS
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 6044-1 : 200P1 AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS
I.S. EN ISO 14126:2000 FIBRE-REINFORCED PLASTIC COMPOSITES - DETERMINATION OF COMPRESSIVE PROPERTIES IN THE IN-PLANE DIRECTION
SAE AMS 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS
BS EN ISO 14126:1999 Fibre-reinforced plastic composites. Determination of compressive properties in the in-plane direction
ISO 14126:1999 Fibre-reinforced plastic composites — Determination of compressive properties in the in-plane direction
EN ISO 14126:1999/AC:2002 FIBRE-REINFORCED PLASTIC COMPOSITES - DETERMINATION OF COMPRESSIVE PROPERTIES IN THE IN-PLANE DIRECTION

PREN 2489 : 1988 FIBRE REINFORCED PLASTICS - DETERMINATION OF THE ACTION OF LIQUID CHEMICALS
PREN 2743 : 200P1 AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING
PREN 2859 : 1 AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, CLOSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN ALLOY STEEL, CADMIUM PLATED - CLASSIFICATION: 1 100 MPA (AT AMBIENT TEMPERATURE)/235 DEGREES C
PREN 2565 : 200P2 AEROSPACE SERIES - PREPARATION OF CARBON FIBRE REINFORCED RESIN PANELS FOR TEST PURPOSES
PREN 2823 : 200P2 AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS
PREN 3783 : 200P1 AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES
EN 2744:1992 Aerospace series - Non metallic materials - Preferred test temperatures

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Hardcopy - English
PDF - English
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