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Pratt & Whitney XH-3130
From Wikipedia, the free encyclopedia
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The Pratt & Whitney XH-3130 (sometimes called the XL-3130[citation needed]) was an H-block aircraft engine project developed for the United States Navy in the late 1930s.[1] The design was later enlarged as the XH-3730), but the project was canceled in 1940 in favor of Pratt & Whitney developing the R-4360 Wasp Major air-cooled radial engine.[2]
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Specifications
General characteristics
- Type: 24 cylinder H-engine
- Bore: 6.00 in (152.4 mm)
- Stroke: 5.50 in (139.7 mm)
- Displacement: 3,732.2 cu in (61.16 L)
Components
Performance
- Power output: 2,900 hp
See also
Related development
Comparable engines
Related lists
References
External links
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