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Aichi Atsuta 31, Ha 60 Model 31, V-12 Engine

Air and Space Museum

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International media Interoperability Framework
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  • Side view of pale gray metal engine. Six holes in the side with black wiring coming out of them.
  • Side view of pale gray metal engine. Six holes in the side with black wiring coming out of them.
  • Three quarters view of pale gray metal engine. Crank shaft, wiring, and six holes visible.
  • Pale gray metal engine with six holes in the side. The numbers 197 927 are on the black metal base holding the engine.
  • Three quarters frontal view of the pale gray engine. There is wiring and a shaft driven by a crank on the front.
  • Angled view of the back of the pale gray engine. Tubing, screws, and other machinery visible.
  • Back view of the pale gray engine. Pipes and wiring feature prominently.

    Object Details

    Manufacturer

    Aichi Aircraft Company (Aichi Kokuki KK)

    Designer

    Daimler-Benz Aktiengesellschaft

    Physical Description

    Type: Reciprocating, Inverted V, 12 cylinders, liquid cooled, supercharged, fuel injected
    Power rating: 1,044 kW (1,400 hp) at 2,800 rpm
    Displacement: 33.9 L (2,069 cu in)
    Bore and Stroke: 150 mm (5.91 in.) x 160 mm (6.30 in.)
    Weight: 715 kg (1,576 lb)

    Summary

    The Atsuta 31 was a licensed version of the Daimler-Benz DB 601A liquid-cooled, inverted V-12 engine. The Atsuta reduced an aircraft’s frontal area, increasing aerodynamic efficiency. Aichi manufactured 873 Atsuta series engines during World War II.
    The Atsuta was the only liquid-cooled engine used operationally by the Japanese naval air force. The Ha 60 Model 31 powered the Aichi M6A1 Seiran, a submarine-borne floatplane bomber, and early versions of the Yokosuka D4Y2 series Suisei carrier-based dive bomber and reconnaissance aircraft.

    Credit Line

    Transferred from the U.S. Navy

    Date

    1945

    Inventory Number

    A19710927000

    Restrictions & Rights

    Usage conditions apply

    Type

    PROPULSION-Reciprocating & Rotary

    Materials

    Bearings - Steel backed copper lead
    Crankshaft - Ni/Cr Steel
    Cylinder blocks - Silicon aluminum alloy
    Ignition leads - Fabric covered
    Pistons - Similar to 24S aluminum

    Dimensions

    Length 215.0 cm (84 5/8 in.), Width 71.2 cm (28 1/16 in.), Height 106.0 cm (41 3/4 in.)

    Country of Origin

    Japan

    See more items in

    National Air and Space Museum Collection

    Location

    Steven F. Udvar-Hazy Center in Chantilly, VA

    Hangar

    Boeing Aviation Hangar

    Data Source

    National Air and Space Museum

    Metadata Usage

    Not determined

    Link to Original Record

    http://n2t.net/ark:/65665/nv968e166a8-5513-496a-97dd-b3a5e0620c32

    Record ID

    nasm_A19710927000

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    Propulsion

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