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Catalog Data

Manufacturer:
Curtiss Aeroplane and Motor Company  Search this
Materials:
Aluminum, Steel, Copper, Ceramic, Rubber, Magnesium, Preservative coating
Dimensions:
Height 88.4 cm (34.8 in.), Length 144.3 cm (56.8 in.), Width 71.9 cm (28.3 in.)
Type:
PROPULSION-Reciprocating & Rotary
Country of Origin:
United States of America
Date:
Circa 1921
Physical Description:
Type: Reciprocating, V-type, 12 cylinders, liquid-cooled
Power rating: 242 kW (325 hp) at 1,800 rpm
Displacement: 18.8 L (1,145.09 cu in.)
Bore and Stroke: 114 mm (4.5 in.) x 152 mm (6 in.)
Weight: 437.7 kg (964 lb)
Summary:
The CD-12 (Curtiss Direct-Drive) history extended over several years. Development began in 1915 with the K-12, using the historic design skills of Charles Kirkham; and in competition with the popular Hispano-Suiza. The high power and low weight goal was a great challenge. So it was not surprising that the aluminum monoblock and several other advanced features, including the reduction gearing, presented substantial problems. Unable to overcome these difficulties, Kirkham left Curtiss in 1919, and his successor, Arthur Nutt produced a derated CD-12, without the reduction gearing of the K-12, in 1921.
This artifact was a production prototype, while the other three in its series were sold to the U.S. Navy. In November, 1921, the Navy Curtiss Racer CR-1, powered by a Curtiss CD-12 engine, won the Pulitzer Trophy. CD-12 engines also powered the Curtiss CT Torpedodropper and Navy Curtiss 18T triplane racer. Further development produced the 1922 D-12, a successful engine for both racing and fighter aircraft.
Credit Line:
Transferred from the U.S. Navy
Inventory Number:
A19710888000
Restrictions & Rights:
Usage conditions apply
See more items in:
National Air and Space Museum Collection
Data Source:
National Air and Space Museum
GUID:
http://n2t.net/ark:/65665/nv92fc45606-8231-4e5d-924b-98b463e82ef8
EDAN-URL:
edanmdm:nasm_A19710888000