The Pratt & Whitney R-1535 Twin Wasp Junior was an engine used in American aircraft in the 1930s. The engine was introduced in 1932 as a 14-cylinder version of the 9-cylinder R-985. It was a two-row, air-cooled radial design. Displacement was 1,535 cu in (25.2 l); bore and stroke were both 5+3⁄16 in (132 mm).
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Pratt & Whitney aircraft engines | |
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Radial engines |
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H piston engines |
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Free-piston gas turbines |
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Turbojets |
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Turbofans | |
Turboprops/Turboshafts |
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Propfans |
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Rocket engines |
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Aeroderivative gas turbine engines |
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Subsidiaries |
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Key people |
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† Joint development aeroengines See also: Pratt & Whitney Canada aeroengines |
United States military piston aircraft engine designation system | |
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H (four-bank H-configuration inline) | |
IV (inverted-V inline) | |
L (single-bank inline) | |
O (opposed) | |
R (radial) |
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V (upright-V inline) | |
V (inverted-V inline) | |
VG (inverted-V inline) | |
W (three-bank W-configuration inline) |
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