Pratt & Whitney R-1535 Twin Wasp Junior

1930s American aircraft engine From Wikipedia, the free encyclopedia

The Pratt & Whitney R-1535 Twin Wasp Junior is an American aircraft engine developed in the 1930s. The engine was introduced in 1932 as a 14-cylinder version of the 9-cylinder R-985, and was a two-row, air-cooled radial design. Displacement was 1,535 cu in (25.2 L); bore and stroke were both 5+316 in (132 mm).[1]

National originUnited States
First run1932
Quick facts R-1535 Twin Wasp Junior, Type ...
R-1535 Twin Wasp Junior
Pratt & Whitney Twin Wasp Junior, at the National Museum of Naval Aviation, Pensacola, Florida
TypeRadial engine
National originUnited States
ManufacturerPratt & Whitney
First run1932
Major applications
Developed fromPratt & Whitney R-985 Wasp Junior
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Variants

The following is a representative list of R-1535 variants. Data from a Pratt & Whitney designated-engine index and the U.S. Navy Aeronautical Engine Laboratory report index, unless otherwise noted.[2][3]

  • R-1535-11 - 750 hp (560 kW)
  • R-1535-13 - 750 hp (560 kW), 825 hp (615 kW)
  • R-1535-44 - 625 hp (466 kW)
  • R-1535-64 - 950 hp (710 kW)
  • R-1535-72 - 700 hp (520 kW) for takeoff; 650 hp (480 kW) normal at 7,500 ft (2,300 m)
  • R-1535-82 - 750 hp (560 kW)
  • XR-1535-86 - 825 hp (615 kW); experimental fuel-injection variant
  • XR-1535-88 - 825 hp (615 kW)
  • R-1535-94 - 825 hp (615 kW)
  • R-1535-96 - 825 hp (615 kW)
  • R-1535-98 - 700 hp (520 kW)
  • R-1535-SB4-G - 825 hp (615 kW)

Applications

Applications from the Aircraft Engine Historical Society, unless otherwise noted.[4]

Engines on display

Specifications (R-1535-SB4-G)

Data from [8]

General characteristics

  • Type: Fourteen-cylinder two-row supercharged air-cooled radial engine
  • Bore: 5+316 in (131.8 mm)
  • Stroke: 5+316 in (131.8 mm)
  • Displacement: 1,534.9 cu in (25.153 L)
  • Length: 53.27 in (1,353 mm)
  • Diameter: 44.13 in (1,121 mm)
  • Dry weight: 1,087 lb (493 kg)

Components

Performance

See also

References

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