Object Details
Manufacturer
Allison Division, General Motors Corporation
Physical Description
Type: Reciprocating, 24 cylinders, liquid-cooled,
Power rating: 1,939 kW (2,600 hp) at 3,000 rpm
Displacement: 56 L (3,420 cu in.)
Bore and Stroke: 140 mm (5.5 in.) x 140 mm (5.5 in.)
Weight: 1,485.5 kg (3,275 lb)
Summary
Originally known for modified Liberty engines, the V-1710 was the first truly Allison engine, and became the first American engine to qualify at 746 kW (1,000 horsepower) for the 150-hour military type test. It was the only liquid cooled engine that saw service in World War II, powering most war time U.S. Army fighters, including the P-38, P-39, P-40, P-63, and early P-51s.
In 1937, Allison began development of the V-3420, comprised of two V-1710 engines geared together on a common crankcase. This project resulted from an Army Air Corps interest in a 1,500 kW (2,000 hp) bomber engine. However, development was not pressed until late in the war because of the need for improving the V-1710. Plans were made for producing the V-3420 in large quantity for a high-speed, low-altitude fighter, the Fisher P-75, but only about 100 engines were produced before the project was dropped.
This engine powered the Fisher XP-75A and P-75A.
Credit Line
Transferred From USAAF
Date
Circa World War II
Inventory Number
A19660386000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Reciprocating & Rotary
Materials
Aluminum, Steel, Magnesium, Paint, Copper, Rubber, Wood, Phenolic, Preservative coating
Dimensions
Height 104 cm (40.9 in.), Width 152.2 cm (59.9 in.), Depth 685.8 cm (270 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
Link to Original Record
Record ID
nasm_A19660386000