Pratt & Whitney R-1340 Wasp
The Pratt & Whitney R-1340 Wasp was a reciprocating engine widely used in American aircraft from the 1920s onward. It was the company's first engine, and the first of the famed Wasp family.[1] It was a single-row, nine-cylinder air-cooled radial design, and displaced 1,344 cubic inches (22 L); bore and stroke were both 5.75 in (146.05 mm). A total of 34,966 engines were produced.[2]
Variants
- R-1340-7 — 450 hp (336 kW), 600 hp (447 kW)
- R-1340-8 — 425 hp (317 kW)
- R-1340-9 — 450 hp (336 kW), 525 hp (391 kW)
- R-1340-16 — 550 hp (410 kW)
- R-1340-17 — 525 hp (391 kW)
- R-1340-19 — 600 hp (447 kW)
- R-1340-19F — 600 hp (447 kW)
- R-1340-21G — 550 hp (410 kW)
- R-1340-22 — 550 hp (410 kW)
- R-1340-23 — 575 hp (429 kW)
- R-1340-30 — 550 hp (410 kW)
- R-1340-31 — 550 hp (410 kW)
- R-1340-33 — 600 hp (447 kW)
- R-1340-48 — 600 hp (447 kW)
- R-1340-49 — 600 hp (447 kW)
- R-1340-AN1 — 550 hp (410 kW), 600 hp (447 kW)
- R-1340-AN2 — 550 hp (410 kW), 3:2 geared prop shaft
- R-1340-B — 450 hp (336 kW)
- R-1340-D — 500 hp (373 kW)
- R-1340-S1H1-G — 550 hp (410 kW), 600 (447 kW)
- R-1340-S3H1 — 600 hp (447 kW)
Applications
Specifications (R-1340-S3H1)
Data from [3]
General characteristics
- Type: Nine-cylinder single-row supercharged air-cooled radial engine
- Bore: 5.75 in (146 mm)
- Stroke: 5.75 in (146 mm)
- Displacement: 1,343.8 in3 (22.02 l)
- Length: 44.06 in (1,119 mm)
- Diameter: 51.38 in (1,305 mm)
- Dry weight: 805 lb (365 kg)
Components
Performance
See also
References
Notes
Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
External links
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