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  • ASTM E 103 : 2017 : REDLINE

    Current The latest, up-to-date edition.

    Standard Practice for Rapid Indentation Hardness Testing of Metallic Materials

    Available format(s):  PDF

    Language(s):  English

    Published date:  01-04-2017

    Publisher:  American Society for Testing and Materials

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    Abstract - (Show below) - (Hide below)

    CONTAINED IN VOL. 03.01, 2017 Defines a procedure for rapid indentation hardness testing of metallic materials.

    Scope - (Show below) - (Hide below)

    1.1This practice covers a procedure for rapid indentation hardness testing of metallic materials.

    1.2This practice includes additional requirements in Annex A1 for the direct, indirect, and daily verification of rapid indentation hardness testing machines.

    1.3The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.

    1.4This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

    1.5This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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

    Committee E 28
    Document Type Redline
    Publisher American Society for Testing and Materials
    Status Current

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

    MIL P 64008 : 0 PROJECTILE, 155MM: XM825 METAL PARTS ASSEMBLY
    MIL-P-50345 Revision F:1994 PROJECTILES,155MM:M483A1-M718/M741-M692/M731 METAL PARTS ASSEMBLY
    MIL-DTL-60547 Revision G:2008 PROJECTILE, 105 MM, HE, M1 AND M760 - METAL PARTS ASSEMBLY
    SAE AMS 5663 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1775 DEGREES F (968 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED
    MIL P 60584 : A PROJECTILE, 155MM, SMOKE, WP, M110 METAL PARTS ASSEMBLY
    MIL-DTL-63245 Revision C:2008 Projectile 155 Millimeter: HE, Metal Parts Assembly, M795
    SAE AMS 5442 : 2017 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, NI - 18CR - 2.8MO - 5.5CB(NB) - 0.70TI - 1.50AL - 10FE - 9CO - 1W, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED
    MIL-P-70524 Base Document:1990 PROJECTILE, 105 MM, HE, RA, XM913/XM927 WARHEAD INSULATION ASSEMBLY FOR
    SAE AMS H 6088 : 2000 HEAT TREATMENT OF ALUMINUM ALLOYS
    MIL-DTL-60584 Revision B:2006 Projectile,155 Millimeter - Smoke, WP, Metal Parts Assembly, M110A2
    SAE AMS 7490 : 2014 RINGS, FLASH WELDED, CORROSION AND HEAT-RESISTANT AUSTENITIC STEELS, AUSTENITIC-TYPE IRON, NICKEL, OR COBALT ALLOYS, OR PRECIPITATION-HARDENABLE ALLOYS
    SAE AMS 5962 : 2012 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, ROUND BARS AND WIRE, 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION TREATED AND WORK STRENGTHENED, PRECIPITATION HARDENABLE
    SAE AMS 5441 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, NI - 18CR - 2.8MO - 5.5CB(NB) - 0.70TI - 1.50AL - 10FE - 9CO - 1W, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE
    MIL-H-6088 Revision G:1991 HEAT TREATMENT OF ALUMINIUM ALLOYS
    MIL P 14824 : B PROJECTILE, H.E., 155MM, M107 METAL PARTS ASSEMBLY
    SAE AMS 5884 : 2016 IRON-NICKEL ALLOY, BARS, FORGINGS, AND RINGS, 42FE - 37.5NI - 14CO - 4.8CB(NB) - 1.6TI, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE MULTIPLE MELTED, HIGH TEMPERATURE, LOW EXPANSION
    MIL-P-48323 Revision C:1984 PROJECTILE, 8 INCH, HE, RA, M650 ROCKET MOTOR BODY ASSEMBLY
    SAE AMS 5662 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AI - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE
    MIL-DTL-14824 Revision C:2007 PROJECTILE 155 MM, HE, METAL PARTS ASSEMBLY, M107
    MIL-P-70612 Revision A:1993 PROJECTILE, 155MM, XM864 BASE ASSEMBLY FOR
    ASTM A 880 : 1995 Standard Practice for Criteria for Use in Evaluation of Testing Laboratories and Organizations for Examination and Inspection of Steel, Stainless Steel, and Related Alloys (Withdrawn 2004)

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

    ISO/IEC 17025:2005 General requirements for the competence of testing and calibration laboratories
    ASTM E 10 : 2017-05 TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS
    ISO/IEC 17011:2004 Conformity assessment General requirements for accreditation bodies accrediting conformity assessment bodies
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