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  • EN 2329 : 1993

    Current The latest, up-to-date edition.

    AEROSPACE SERIES - TEXTILE GLASS FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF MASS PER UNIT AREA

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    Language(s): 

    Published date:  03-03-1993

    Publisher:  Comite Europeen de Normalisation

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

    Cooperating organizations
    National foreword
    Foreword
    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
    National annex NA (informative) Committees responsible

    Abstract - (Show below) - (Hide below)

    This standard specifies a method for determining the mass per unit area of a textile glass fibre preimpregnate, for aerospace use.

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

    Development Note Supersedes PREN 2329. (11/2003)
    Document Type Standard
    Publisher Comite Europeen de Normalisation
    Status Current
    Supersedes

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

    93/706616 DC : 0 PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL
    PREN 3783 : 200P1 AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES
    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
    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
    PREN 2833-1 : 200P2 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: 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
    BS EN 3783:2013 Aerospace series. Fibre composite materials. Normalisation of fibre dominated mechanical properties
    SAE AMS 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS
    I.S. EN 3783:2013 AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES
    EN 2331 : 1993 AEROSPACE SERIES - TEXTILE GLASS FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN AND FIBRE CONTENT AND MASS OF FIBRE PER UNIT AREA
    EN 3783:2013 Aerospace series - Fibre composite materials - Normalisation of fibre dominated mechanical properties
    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]
    UNI EN 3783 : 2014 AEROSPACE SERIES - FIBRE COMPOSITE MATERIALS - NORMALISATION OF FIBRE DOMINATED MECHANICAL PROPERTIES

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

    PREN 2743 : 200P1 AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING
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