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Rolls-Royce Goshawk

From Wikipedia, the free encyclopedia
1930s British piston aircraft engine

Goshawk
TypePistonV-12aero engine
ManufacturerRolls-Royce Limited
First run1933
Major applicationssee#Applications
Number built20
Developed fromRolls-Royce Kestrel

TheRolls-Royce Goshawk was a development of theRolls-Royce Kestrel that usedevaporative or steam cooling. In line with Rolls-Royce convention of naming piston engines afterbirds of prey, it was named after thegoshawk.

The engine first ran in 1933 and provided 660horsepower (490 kW). Only a few engines were built as the aircraft designs intended to use it were not adopted by theRoyal Air Force. The Goshawk was used to power theShort Knuckleduster, theSupermarine Type 224 (a predecessor to theSupermarine Spitfire) and other prototype aircraft.

Design and development

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The Goshawk was developed from theKestrel IV prototype engine, to useevaporative (also known as "steam") cooling. Rather than keep the cooling liquid below its boiling point in the cooling system, the coolant was allowed to boil; the phase change from liquid to vapour takes more heat from the engine, so less weight of coolant is needed. However, the radiator had to be bulkier to accommodate coolant in its gas phase, which increased drag.

Twenty engines were built, and flew only in prototypes as a few manufacturers' private ventures and "one-offs". Powers for individual installations are quoted between 650 and 700 hp (520 kW). Problems with coolant leaks, coolant pumping and the realisation that large wing-mounted condensing radiators would be vulnerable to combat damage caused the project to be cancelled, although valuable lessons had been learned and were put to good use with development of the laterMerlin.[1]

Variants

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Goshawk I
(1932) Developed from the prototype Kestrel IV.
Goshawk II
(1935) 600 hp. Lowered propeller reduction gear ratio.
Goshawk III
(1935) 600hp. Further reduction of gear ratio.
Goshawk VI
660 hp. High ratio reduction gear.
Goshawk VII
660 hp. Raised reduction gear ratio.
Goshawk VIII
660 hp. Special experimental engine. Maximum power output: 837 hp.

Applications

[edit]
Goshawk powered Short Knuckleduster

The Goshawk was the power unit specified for the twin engined Short Knuckleduster flying boat (K3574) to Specification R24/31 and "preferred" for submissions to Air Ministry specification F7/30 for a fighter aircraft. Goshawks were used by all three officially sponsored prototypes, theSupermarine Type 224 (K2890),theWestland F.7/30 (K2891) and theBlackburn F3 (K2892), which only taxied with the Goshawk fitted and did not fly, in addition to two private venture entrants, theBristol Type 123 and theHawker P.V.3.

The Goshawk also powered Hawker's privately developed "High Speed Fury Mk 2" (K3586) and "Intermediate Fury" 2" (the latter Hawker's own development aircraft and "hack" serialG-ABSE)[2] and theWestland Pterodactyl V (K2770) and was installed for trials in theGloster TSR.38 (S1705), and the firstGloster Gnatsnapper prototype (N227).

Application list

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Specifications (Goshawk I)

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Data fromLumsden[3]

General characteristics

  • Type: 12-cylinder liquid-cooled 60 degreeVee aircraft piston engine
  • Bore: 5.0 in (127 mm)
  • Stroke: 5.5 in (140 mm)
  • Displacement: 1,295.88 in3 (21.25 L)
  • Length: 74.61 in (1,895 mm)
  • Width: 24.41 in (620 mm)
  • Height: 35.63 in (905 mm)
  • Dry weight: 975 lb (442 kg)

Components

Performance

See also

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Related development

Comparable engines

Related lists

References

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Notes
  1. ^Gunston 1989, p.141.
  2. ^"Fighting Breed" Flight 1951 p692
  3. ^Lumsden 2003, p.197.
Bibliography
  • Gunston, Bill.World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.ISBN 1-85260-163-9
  • Lumsden, Alec.British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003.ISBN 1-85310-294-6.
  • "The Two Rs"Flight 1954 from archive at Flightglobal.com

Further reading

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  • Rubbra, A.A.Rolls-Royce Piston Aero Engines - a designer remembers: Historical Series no 16 :Rolls-Royce Heritage Trust, 1990.ISBN 1-872922-00-7
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