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McCulloch TSIR-5190

From Wikipedia, the free encyclopedia
McCulloch TSIR-5190
Type Air-cooled five-cylinder radial piston aircraft engine
National origin United States
Manufacturer McCulloch Motors Corporation

The TSIR-5190 is a five cylinder two-stroke radial piston aircraft engine developed for aircraft applications by McCulloch Motors Corporation.

Joe Crover and his father patented new technologies to complete development of the engine for production use. A pair of TRAD-4180s four cylinder diesels and a single TSIR-5190 from the Western Museum of Flight are in use for development.[1]

Specifications (TSIR-5190)

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General characteristics

Components

  • Oil system: dry sump
  • Cooling system: liquid cooled

Performance

  • Power output: 270 hp (201 kW) @ 3600 rpm

References

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  1. ^ "Older Diesel Engine Gets Another Look". AOPA Pilot: 48. March 2015.
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