Skip to content
Please enter a keyword to search

  • PREN 6062 : 200P1

    Current The latest, up-to-date edition.

    AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - FLATWISE TENSILE TEST OF COMPOSITE SANDWICH PANEL

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  30-11-1995

    Publisher:  Aerospace & Defence Industries Association of Europe

    Add To Cart

    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

    Abstract - (Show below) - (Hide below)

    Gives the flatwise tensile test, which is the procedure for the determination of the tensile strength, perpendicular to the honeycomb sandwich panels. The specimen is designed to fail in one of the core to skin bonds. Also can be used to obtain compatibility and strength data on unidirectional and woven fabric laminates, structural adhesives and epoxy resin used for repair purposes.

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

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

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

    SAE AMS 2950/1 : 2008 PASTE ADHESIVE FOR CORE RESTORATION - 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 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS
    SAE AMS 2950/1 : 2008(R2019) PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS

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

    PREN 2743 : 200P1 AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING
    PREN 2823 : 200P2 AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS
    PREN 2419 : 200P3 AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T351 - PLATE - 6 MM < A <= 80 MM
    PREN 2334 : 1995 CHROMIC-SULPHURIC ACID PICKLE OF ALUMINIUM AND ALUMINIUM ALLOYS
    View more information

    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective