Object Details
Manufacturer
Pratt & Whitney
Physical Description
Type: Reciprocating, 18 cylinders, 2 rows, radial, air-cooled
Power rating: 1,491 kW (2,000 hp) at 2,700 rpm
Displacement: 45.9 L (2,800 cu in.)
Bore and Stroke: 146 mm (5.8 in.) x 152 mm (6.0 in.)
Weight: 1,043 kg (2,300 lb)
Summary
Pratt & Whitney initiated design and development of the R-2800 Double Wasp in 1936, and first displayed it in 1939 at the New York World’s Fair. With water injection and turbo-supercharging, the R-2800 produced more than one-horsepower per 16.4 cc (cubic inch). Thin, highly pitched cooling fins machined directly from the head forging solved the heat dissipation problem. When introduced, it produced the greatest output at altitude of any engine in the world.
During World War II, it powered the Grumman F6F Hellcat, Vought F4U Corsair, Republic P-47 Thunderbolt, and other combat aircraft. After the War, it was chosen to power the Douglas DC-6 and other airliners. When production ended in 1960, more than 125,000 R-2800s had been manufactured by Pratt & Whitney and it licensees, one of the largest production runs of any single aircraft engine model.
This R-2800-43 model powered the Martin AT-23A, B-26B/C/E/F/G, XB-26D, TB-26G, XB-26H, and Curtiss C-46.
Credit Line
Transferred from USAAF
Date
1939
Inventory Number
A19660391000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Reciprocating & Rotary
Materials
Aluminum
Steel
Magnesium Alloy
Paint
Cotton
Copper Alloy
Cadmium Plating
Plastic
Porcelain
Rubber
Dimensions
Diameter 133.4 cm (52.5 in.), Length 192.3 cm (75.7 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_A19660391000