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Rolls Royce Hawk

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Rolls-Royce Hawk

The Rolls-Royce Hawk was a British aero engine designed by Rolls-Royce in 1915. Derived from one bank of six cylinders of the Rolls-Royce Eagle, it produced 75 horsepower at 1,370 rpm. Power was progressively increased to 91 hp by February 1916, and 105 hp by October 1918.

Contents

After Rolls-Royce made the prototypes, the Hawk was manufactured under licence by Brazil Straker in Bristol between 1915 and 1918. During this period 204 engines were built, and the Hawk earned a reputation for high reliability.

Many engines of this type were used to power the SSZ class coastal patrol airships of which 76 were built.

Applications

  • Avro 504F
  • Farman MF.7
  • Royal Aircraft Factory B.E.2
  • SS class blimp (1 example)
  • SSP class blimp
  • SSZ class blimp
  • SST class blimp
  • Specifications (Hawk I)

    Data from Lumsden

    General characteristics

  • Type: 6-cylinder liquid-cooled inline aircraft piston engine
  • Bore: 4 in (101.6 mm)
  • Stroke: 6 in (152.4 mm)
  • Displacement: 452.3 inĀ³ (7.41 L)
  • Length: 46.85 in (1190 mm)
  • Width: 23.5 in (597 mm)
  • Height: 35.5 in (902 mm)
  • Dry weight: 387 lb (175.5 kg)
  • Components

  • Valvetrain: OHC - Overhead camshaft
  • Fuel system: Twin Claudel-Hobson FZR carburettors
  • Fuel type: Petrol
  • Cooling system: Liquid-cooled
  • Performance

  • Power output: 75 hp (56 kW) at 1,350 rpm
  • Compression ratio: 5.1:1
  • Power-to-weight ratio: 0.2 hp/lb (0.3 kW/kg)
  • References

    Rolls-Royce Hawk Wikipedia