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  • MIL STD 401 : B

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    SANDWICH CONSTRUCTIONS AND CORE MATERIALS, GENERAL TEST METHODS

    Available format(s):  Hardcopy, PDF

    Superseded date:  01-06-1999

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Provisions and methods for testing sandwich core materials and construction for use in aircraft structures.

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

    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded

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

    MIL C 8087 : C CORE MATERIAL, FOAMED IN PLACE, URETHANE TYPE
    MIL L 81293 : A LIGHTWEIGHT SANDWICH CONSTRUCTED PANEL (ASROC) LAUNCHER MK 112
    MIL C 7438 : G CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION
    MIL S 9041 : B SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS
    MIL S 25392 : B SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND POLYURETHANE FOAMED-IN-PLACE CORE, FOR AIRCRAFT STRUCTURAL APPLICATIONS
    MIL E 87235 : 0 EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
    MIL STD 1547 : B ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES
    MIL R 7705 : B RADOME, GENERAL SPECIFICATION FOR
    MIL S 29413 : B SHELTER, JOINING CORRIDOR FOR
    DIN 65067-1:1980-12 AEROSPACE; SANDWICH STRUCTURES WITH TOP LAYERS OF FIBRE REINFORCED PLASTICS, TECHNICAL SPECIFICATION
    MIL S 29410 : B SHELTER ASSEMBLY, RIGID GENERAL PURPOSE
    SAE AMS C 8073 : 2013 CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED GLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS
    MIL M 81957 : B MOBILE TEST FACILITY, GAS TURBINE ENGINE TEST SYSTEMS - GENERAL SPECIFICATION FOR
    MIL S 29411 : B SHELTER ASSEMBLIES, 10 FOOT AND 20 FOOT ELECTROMAGNETIC INTERFERENCE
    SAE AMS C 81986 : 1998 CORE MATERIAL, PLASTIC HONEYCOMB, NYLON PAPER BASE; FOR AIRCRAFT STRUCTURAL APPLICATIONS
    MIL C 81986 : 0 CORE MATERIAL, PLASTIC HONEYCOMB, NYLON PAPER BASE; FOR AIRCRAFT STRUCTURAL APPLICATIONS
    MIL P 43184 : 0 PLATFORM COMPONENTS, AIR DELIVERY. MODULAR (DUAL RAIL SYSTEM), TYPE II
    ASTM E 1555 : 2012 : REDLINE Standard Specification for Structural Paste Adhesive for Sandwich Panel Repair
    DIN 65090:1979-07 AEROSPACE; TEXTILE GLASS, PREIMPREGNATED FILAMENT GLASS CLOTH FROM E-GLASS (PREPREG), TECHNICAL SPECIFICATIONS
    ASTM E 1091 : 2013 : REDLINE Standard Specification for Nonmetallic Honeycomb Core for Use in Shelter Panels
    MIL C 8073 : D CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED CLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS
    NASA MSFC STD 506 : 1988 MATERIALS AND PROCESSES CONTROL
    MIL P 43772 : A PANEL TYPE II MODULAR PLATFORM, AIRDROP

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

    ASTM C 271 : 1999 Standard Test Method for Density of Sandwich Core Materials
    ASTM C 393 : 2000 Standard Test Method for Flexural Properties of Sandwich Constructions
    ASTM D 1781 : 1998 Standard Test Method for Climbing Drum Peel for Adhesives
    ASTM C 297 : 1994 : R1999 Standard Test Method for Flatwise Tensile Strength of Sandwich Constructions
    ASTM C 363 : 2000 Standard Test Method for Delamination Strength of Honeycomb Core Materials
    MIL STD 105 : E SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES
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