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  • PREN 6043 : 200P1

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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 - THERMOSETTING RESIN SYSTEMS - TEST METHOD - DETERMINATION OF GEL TIME AND VISCOSITY

    Available format(s):  Hardcopy, PDF

    Withdrawn date:  23-07-2013

    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 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
    Annex A - Equipments

    Abstract - (Show below) - (Hide below)

    Gives the procedure for the determination of the viscosity and gel time of thermosetting resin systems by using several experimental techniques. The results obtained under dynamic and/or isothermal conditions, may be used to control the processing of resin systems during the cure cycle.

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

    Comment Closes On
    Committee AIB/TF6
    Document Type Draft
    Publisher Aerospace & Defence Industries Association of Europe
    Status Withdrawn

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

    PREN 6085 : 200P1 AEROSPACE SERIES - NON-METALLIC MATERIALS - EPOXY SURFACING FILMS
    PREN 6084 : 200P1 AEROSPACE SERIES - NON-METALLIC MATERIALS - SURFACING FILMS - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS
    SAE AMS 3970/3 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 3: PURCHASING SPECIFICATION FOR CARBON PREPREG
    PREN 2833-1 : 200P2 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS
    PREN 6044-1 : 200P1 AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - 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
    SAE AMS 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES 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]
    SAE AMS 3970/4 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 4: PURCHASING SPECIFICATION FOR FILM ADHESIVE
    SAE AMS 2950/1 : 2008 PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS
    SAE AMS 2950/1 : 2008(R2019) PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS
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