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Armstrong Siddeley Panther

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(Redirected from Armstrong Siddeley Panther IIA) 1920s British piston aircraft engine

Panther/Jaguar Major
Type Radial engine
National origin United Kingdom
Manufacturer Armstrong Siddeley
First run 1929
Major applications Fairey Gordon

The Armstrong Siddeley Panther was a 27-litre 14-cylinder twin-row air-cooled radial aero engine developed by Armstrong Siddeley. It was originally named the Jaguar Major.

Variants

This list is incomplete; you can help by adding missing items. (November 2023)
AS Panther IIIA
500 hp (370 kW)
AS Panther VII
638 hp (478 kW) at 2,400 rpm with 0.5 psi (3.5 kPa) boost

Applications

Specifications (Panther VII)

Data from

General characteristics

  • Type: 14-cylinder twin-row air-cooled radial engine
  • Bore: 5.25 in (133.4 mm)
  • Stroke: 5.5 in (139.7 mm)
  • Displacement: 1,667 cu in (27.3 L)
  • Length: 64 in (1.63 m)
  • Diameter: 46.45 in (1.18 m)
  • Dry weight: 1,047 lb (475 kg)

Components

Performance

See also

Related development

Related lists

References

Notes

  1. Lumsden 2003, p.72.
  2. Lumsden 2003, p.73.

Bibliography

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
Armstrong Siddeley aero engines
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