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  • PREN 2850 : 200P2

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    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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    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    Withdrawn date:  11-12-2023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

    Published date: 

    Publisher:  Aerospace & Defence Industries Association of Europe

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

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

    General Product Information - (Show below) - (Hide below)

    Comment Closes On
    Committee C7
    Document Type Draft
    Product Note Superseded by EN 2850:2017
    Publisher Aerospace & Defence Industries Association of Europe
    Status Withdrawn
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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