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Sopwith Dragon - Wikipedia, the free encyclopedia

Sopwith Dragon

From Wikipedia, the free encyclopedia

Sopwith Dragon
Type Single-seat fighter biplane
Manufacturer Sopwith Aviation Company
Maiden flight 1919
Primary user Royal Air Force
Number built 76
Developed from Sopwith Snipe

The Sopwith Dragon was a 1910s British single-seat fighter biplane developed from the Sopwith Snipe by the Sopwith Aviation Company.

[edit] Design and development

First flown in January 1919 the Dragon was a Snipe re-engined with a 320hp (239kW) ABC Dragonfly I radial engine. With an increase of speed from the Snipe it was ordered into production for the Royal Air Force with a larger 350hp (268kW) engine. The Dragon was a two-bay unswept biplane with unequal span wings and ailerons fitted on all four wings and a braced tailplane and a single fin and rudder. It had a fixed tailskid landing gear with a cross-axle type main gear with twin wheels carried on vee legs under the fuselage. It was powered by a nose-mounted 360hp (268kW) ABC Dragonfly IA radial engine driving a two-bladed propeller. It had an open cockpit behind the upper wing and two forward firing Vickers machine-guns mounted above the engine.

The aircraft was not used operationally during the First World War due to the unreliability of the Dragonfly engine.

[edit] Operators

Flag of the United Kingdom United Kingdom

[edit] Specifications

General characteristics

  • Crew: 1
  • Length: 21 ft 9 in (6.63 m)
  • Wingspan: 31 ft 1 in (9.47 m)
  • Height: 9 ft 6 in (2.9 m)
  • Wing area: 271 ft² (25.2 m²)
  • Gross weight: 2132 lb (967 kg)
  • Powerplant: 1 × ABC Dragonfly IA radial engine, 360 hp (268 kW)

Performance

  • Maximum speed: 150 mph (240 km/h)
  • Endurance: 3 hours  30 min
  • Service ceiling: 25,000 ft (7,600 m)

Armament

[edit] See also

Related development

Related lists

[edit] References



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