Fairey Ferret

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Ferret
FFerret.jpg
Ferret Mk.III
Role Two-seat general purpose biplane
National origin United Kingdom
Manufacturer Fairey Aviation Company
First flight June 1925
Number built 3

The Fairey Ferret was a 1930s British general purpose biplane designed and built by the Fairey Aviation Company.[1] It performed well in trials but it was not ordered into production.[1]

Development[edit]

The Ferret was designed to meet a Fleet Air Arm requirement defined by specification 37/22[2] for a reconnaissance aircraft; it was the company's first all-metal design.[1] With a lack of interest from the FAA the company proposed the design to meet a Royal Air Force requirement for a general-purpose biplane.[1]

The company built three prototypes, two were three-seaters (to meet the naval requirement) and the third was a two-seater.[1] The two-seater Ferret III was also fitted with a new Fairey-designed high-speed gun mounting in the rear cockpit.[1] The first prototype first flew in June 1925 powered by a 400hp (298kW) Armstrong Siddeley Jaguar IV radial engine.[1] The other two aircraft had a 9 inch extension to the wing span and were both fitted with a 425hp (317kW) Bristol Jupiter radial engine.[1]

The aircraft performed well during trials at RAF Martlesham Heath but was not ordered into production.[1]

Variants[edit]

Fairey Ferret I
Ferret Mk I
Three-seat prototype powered by a 400hp (298kW) Armstrong Siddeley Jaguar IVl radial engine, one built.[1]
Ferret Mk II
Three-seat prototype powered by a 425hp (317kW) Bristol Jupiter radial engine, one built.[1]
Ferret Mk III
Two-seat prototype powered by a 425hp (317kW) Bristol Jupiter radial engine, one built.[1]

Specifications (Ferret III)[edit]

Data from [1]

General characteristics

  • Crew: 2
  • Length: 29 ft 6 in (8.99 m)
  • Wingspan: 40 ft 7 in (12.37 m)
  • Height: 10 ft 3 in (3.12 m)
  • Wing area: 380 ft2 (35.30 m2)
  • Empty weight: 2,583 lb (1,172 kg)
  • Gross weight: 4,765 lb (2,161 kg)
  • Powerplant: 1 × Bristol Jupiter VI 9-cylinder radial engine, 425 hp (317 kW)

Performance

  • Maximum speed: at 5,000 ft (1,524 m)135 mph (217 km/h)
  • Service ceiling: 15,500 ft (4,725 m)
  • Rate of climb: [2] initial 920 ft/min (4.67 m/s)

Armament

  • 1 × fixed forward-firing 0.303in (7.7mm) Vickers machine-gun (on starboard side of fuselage)
  • 1 × 0.303in (7.7mm) Lewis machine-gun in rear cockpit
  • Up to 500lb (227kg) bombs fitted under wings

References[edit]

Notes[edit]

  1. ^ a b c d e f g h i j k l m Orbis 1985, pp. 1695-1696
  2. ^ a b Taylor & 1974 129-133

Bibliography[edit]