Allison V-1710-33 (V-1710-C15), V-12 Engine
Object Details
- Manufacturer
- Allison Division, General Motors Corporation
- Designer
- Norm Gilman
- Physical Description
- Type: Reciprocating, 12 cylinders, V-type, liquid cooled
- Power rating: 776 kW (1,040 hp) at 2,800 rpm
- Displacement: 28 L (1,710 cu in.)
- Bore and Stroke: 140 mm (5.5 in.) x 152 mm (6 in.)
- Weight (dry): 608 kg (1,340 lb)
- Summary
- In 1937 the Allison V-1710 became the first American engine to qualify at 1,000 horsepower for the new 150-hour military type test. The V-1710-C was also the first in the “long nose” series that provided a basis for later improved and higher powered versions. Allison designers created the long nose by extending the propeller shaft about 30 centimeters (12 inches) to maximize streamlining.
- The Allison V-1710 powered most U.S. Army fighters in World War II, including the Lockheed P-38, Bell P-39 and P-63, Curtiss P-40, and early North American P-51s. The V-1710-C15 (military designation V-1710-33) powered the Curtiss P-40, P-40A, B, and C pursuit aircraft.
- Credit Line
- Lent by Allison Division, General Motors Corporation
- 1939
- Inventory Number
- A19420027000
- Restrictions & Rights
- Usage conditions apply
- Type
- PROPULSION-Reciprocating & Rotary
- Dimensions
- Length 250.3 cm (98.54 in.), Width 74 4 cm (29.29 in.), Height 106.4 cm (41.88 in.)
- Country of Origin
- United States of America
- See more items in
- National Air and Space Museum Collection
- Location
- Steven F. Udvar-Hazy Center in Chantilly, VA
- Hangar
- Boeing Aviation Hangar
- National Air and Space Museum
- Record ID
- nasm_A19420027000
- Metadata Usage (text)
- Not determined
- GUID (Link to Original Record)
- http://n2t.net/ark:/65665/nv99149ad93-6479-411f-b723-5e424519d801
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