Dewoitine D.27

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
D.27
File:Dewoitine D.27.jpg
General information
TypeFighter
ManufacturerDewoitine
Primary userSwiss Air Force
History
Introduction date1931
First flight1928

The Dewoitine D.27 was a parasol monoplane fighter aircraft designed by Émile Dewoitine in 1928.

Design and development

[edit | edit source]

After the end of World War I, the slump in demand for aircraft forced Dewoitine to close his company and move to Switzerland in 1927.

He produced the D.27 the following year, 66 of which were produced for the Swiss Air Force from 1931. It was also license-built in Yugoslavia by Zmaj aircraft and in Romania.

Operational history

[edit | edit source]

Seven strengthened versions, designated the D.53, served experimentally with the French Escadrille 7C1, flying from the aircraft carrier Béarn.

Variants

[edit | edit source]
  • D.271 : One aircraft used for testing a Hispano-Suiza 12Hb engine.
  • D.273 : One aircraft used for testing a Bristol Jupiter engine with supercharger.
  • D.531 : One aircraft used for testing a Hispano-Suiza engine.
  • D.532 : A single aircraft used for testing a Rolls-Royce Kestrel inline engine.
  • D.535 : One aircraft fitted with an HS 12Xbis engine.
  • D.534 : Used for parachute trials.

Operators

[edit | edit source]
File:Flag of France.svg France
File:Flag of Romania.svg Romania
File:Flag of Spain (1931–1939).svg Spain
File:Flag of Switzerland (Pantone).svg Switzerland
File:Flag of Yugoslavia (1918–1943).svg Yugoslavia

Specifications (D.27)

[edit | edit source]
File:Dewoitine D.27 3-view Aero Digest July,1930.png
Dewoitine D.27 3-view drawing from Aero Digest July,1930
File:Dewoitine D27.svg
D.27 6-view. Yugoslav version with metal tail vs. French version. In the middle are the prototype propeller, wooden propeller and metal propeller.

Data from Encyclopedia of Military Aircraft[1]

General characteristics

  • Crew: one
  • Length: 6.5 m (21 ft 4 in)
  • Wingspan: 9.8 m (32 ft 2 in)
  • Height: 2.79 m (9 ft 2 in)
  • Empty weight: 1,038 kg (2,288 lb)
  • Gross weight: 1,382 kg (3,047 lb)
  • Max takeoff weight: 1,414 kg (3,117 lb)
  • Powerplant: 1 × Hispano-Suiza 12Mc V-12 liquid-cooled piston engine, 373 kW (500 hp)

Performance

  • Maximum speed: 312 km/h (194 mph, 168 kn)
  • Range: 600 km (370 mi, 320 nmi)
  • Service ceiling: 9,200 m (30,200 ft)
  • Rate of climb: 10 m/s (2,000 ft/min)

Armament

See also

[edit | edit source]

Lua error in mw.title.lua at line 392: bad argument #2 to 'title.new' (unrecognized namespace name 'Portal'). Related lists

References

[edit | edit source]
  1. ^ Jackson, Robert, The Encyclopedia of Military Aircraft, Paragon, 2002. Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).

Bibliography

[edit | edit source]
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  • Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
[edit | edit source]