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  2. Izod impact strength test - Wikipedia

    en.wikipedia.org/wiki/Izod_impact_strength_test

    The ASTM International standard for Izod Impact testing of plastics is ASTM D256. The results are expressed in energy lost per unit of thickness (such as ft·lb/in or J/cm) at the notch. Alternatively, the results may be reported as energy lost per unit cross-sectional area at the notch (J/m 2 or ft·lb/in 2).

  3. Check weigher - Wikipedia

    en.wikipedia.org/wiki/Check_weigher

    In English units, is this from less than 100th of an ounce to as much as 500 lbs or more. Specialized checkweighers can weigh commercial aircraft, and even find their center-of-gravity. Checkweighers can operate at very high speeds, processing products weighing fractions of a gram at over 100m/m (meters per minute) and materials such as ...

  4. Short ton - Wikipedia

    en.wikipedia.org/wiki/Short_ton

    The short ton (abbreviation tn [1]) is a measurement unit equal to 2,000 pounds (907.18 kg). It is commonly used in the United States, where it is known simply as a ton; [1] however, the term is ambiguous, the single word "ton" being variously used for short, long, and metric tons.

  5. Charpy impact test - Wikipedia

    en.wikipedia.org/wiki/Charpy_impact_test

    The Standard methods for Notched Bar Impact Testing of Metallic Materials can be found in ASTM E23, [8] ISO 148-1 [9] or EN 10045-1 (retired and replaced with ISO 148-1), [10] where all the aspects of the test and equipment used are described in detail.

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  7. Dead-blow hammer - Wikipedia

    en.wikipedia.org/wiki/Dead-blow_hammer

    A dead-blow hammer is a specialized mallet helpful in minimizing damage to the struck surface and in controlling striking force, with minimal rebound from the struck surface. The minimal rebound is helpful in avoiding accidental damage to precision work, especially in tight locations and in applications such as maintenance work on hydraulic ...

  8. Thrust-to-weight ratio - Wikipedia

    en.wikipedia.org/wiki/Thrust-to-weight_ratio

    Take-off can occur when the vehicle's g-force exceeds local gravity (expressed as a multiple of g 0). The thrust-to-weight ratio of rockets typically greatly exceeds that of airbreathing jet engines because the comparatively far greater density of rocket fuel eliminates the need for much engineering materials to pressurize it.

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