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Curtiss K-12, V-12 Engine

Air and Space Museum

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    Object Details

    Manufacturer

    Curtiss Aeroplane and Motor Company

    Physical Description

    Type: Reciprocating, 12 cylinders, V-type, water cooled
    Power rating: 280 kW (375 hp) at 2,250 rpm
    Displacement: 18.8 L (1,145.09 cu in.)
    Bore and Stroke: 114 mm (4.5 in.) x 152 mm (6 in.)
    Weight: 307.5 kg (678 lb)

    Summary

    In 1916 Curtiss engineer Charles Kirkham began designing an engine to compete with the Wright Corporation's Hispano-Suiza. By late 1917, the prototype K-12 (K for Kirkham) was bench tested. While it met its design objectives of high power, low frontal area, compact size, and low weight, the engine encountered technical difficulties during development. Kirkham left Curtiss in 1919, and Arthur Nutt took over the project, eventually producing the D-12, which became a highly successful racing and military power plant in the 1920s.
    This engine is manufacturer's number 5 out of about 20 built. The K-12 powered the Curtiss Navy 18T Wasp triplane and the Army Curtiss 18B Hornet biplane. In 1919 Curtiss test pilot Roland Rholfs set a new world's altitude record of 10,641 m (34,910 ft) with the 18T.

    Credit Line

    Transferred from the U.S. Navy

    Date

    Circa 1918

    Inventory Number

    A19710907000

    Restrictions & Rights

    CC0

    Type

    PROPULSION-Reciprocating & Rotary

    Materials

    Steel, Aluminum, Paint, Preservative coating, Rubber, Ceramic, Copper, Brass, Phenolic

    Dimensions

    Length 152.4 cm (60 in.) (approximate), Width 70.8 cm (27.875 in.), Height 101.9 cm (40.125 in.)

    Country of Origin

    United States of America

    See more items in

    National Air and Space Museum Collection

    Data Source

    National Air and Space Museum

    Metadata Usage

    CC0

    Link to Original Record

    http://n2t.net/ark:/65665/nv97125d33a-36f3-4573-8bf8-f3485f415cbe

    Record ID

    nasm_A19710907000

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