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Thomas-Morse Model 8, V-8 Engine

Air and Space Museum

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    Object Details

    Manufacturer

    Thomas-Morse Aircraft Corporation (Ithaca, New York)

    Physical Description

    Type: Reciprocating, 8 cylinders, V-type,water-cooled
    Power rating: 101 kW (135 hp) at 2,000 rpm
    Displacement: 9.062 L (552.88 cu in.)
    Bore and Stroke: 101.6 mm (4 in.) x 139.7 mm (5.5 in.)
    Weight: 272 kg (600 lb)

    Summary

    The Thomas brothers of Upstate New York began experimenting and flying Curtiss-type aircraft in 1908, and developed their own aircraft in the 1909-10 period. Thomas Brothers aircraft were supplied to the Allied nations during World War I. Airplane engines were built by the Thomas Aeromotor Company, which was later reorganized and became known as the Thomas-Morse Aircraft Corporation of Ithaca, New York. The company's first engine, a 4-cylinder vertical water-cooled design rated at 89.5 kW (120 shp), was produced in 1912. After that, the company confined its efforts entirely to 8-cylinder water-cooled V-types.
    The Thomas-Morse Model 8 engine was fitted with reduction gears to reduce propeller speed to 1,200 rpm. It was the first aircraft engine to be equipped with a self-starter. It powered aircraft such as the Thomas D-5 and L.W.F.

    Credit Line

    Transferred from the War Department, Air Corps, Materiel Division, Wright Field, Dayton, Ohio

    Date

    1917

    Inventory Number

    A19340011000

    Restrictions & Rights

    CC0

    Type

    PROPULSION-Reciprocating & Rotary

    Materials

    Steel, Aluminum, Brass, Copper, Rubber, Stainless steel, Phenolic, Wood

    Dimensions

    Depth 111.8 cm (44 in.), Length 162.6 cm (64 in.), Width 96.5 cm (38 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/nv90194aa77-a4b0-4777-ae60-857470cdda6d

    Record ID

    nasm_A19340011000

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    Propulsion

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