Nieuport 12

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Nieuport 12 and 12bis
Nieuport 12 A.2 prototype
Role Reconnaissance(Artillery)/Fighter/Trainer
Manufacturer Nieuport
Designer Gustave Delage
First flight 1915
Introduction 1915
Status retired
Primary users France
Imperial Russian Air Service
Royal Naval Air Service
Royal Flying Corps
Produced 1915–1918
Number built 300+[1]
Developed from Nieuport 10

The Nieuport 12 (or Nieuport XII in contemporary sources) was a French sesquiplane reconnaissance, fighter aircraft and trainer used by France, Russia, Great Britain and the United States during World War I. Later production examples were built as trainers and served widely until the late 1920s.

Design and development

To improve the performance of the

Vickers gun
for the pilot. Additional modifications were made to those built by Beardmore.

It could be fitted with either a 100 hp (75 kW) Clerget, 130 hp (97 kW) Clerget 9B engine or 110 hp (82 kW) Le Rhône 9J mounted in the nose.

Variants

Nieuport 12bis of Escadrille N69
American Nieuport 80 E.2 trainer
Royal Flying Corps Nieuport 12 built by Beardmore. Elevator stripes were a Beardmore trademark.
Nieuport 12 A.2
Two-seat fighter-reconnaissance biplane, powered by 110 hp (82 kW)
Clerget 9Z engine.[2] or 110 hp (82 kW) Le Rhône 9J
.
Nieuport 12bis C.2
Revised version with 130 hp (97 kW) Clerget 9B engine and streamlined side fairings.[3]
Nieuport 13
Two prototypes with increased span but same nominal wing area as 12. One powered by a 140 hp (100 kW) Hispano-Suiza 8, and the other by an 80 hp (60 kW) Le Rhône 9C.
Nieuport 20
Version powered by 110 hp (82 kW) Le Rhône 9J. Not used by France, but 21 delivered to Royal Flying Corps.[4] All but first examples externally similar to 12bis.
23 meter Nieuport
Unofficial generic designation for all types listed here based on nominal wing area of 23 square meters.
Nieuport 80 E.2 and 81 E.2
Nieuport 12s were later built in large numbers specifically as training aircraft with the gun ring removed. 8 in designation referred to 80 hp (60 kW) Le Rhône 9C. These differed in having flight controls for just the pilot in the rear seat (81 E.2), or both pilot and passenger (80 E.2).
Nieuport 12 (Beardmore)
Beardmore progressively redesigned the Nieuport 12 during a production run of 50 aircraft so early examples were almost stock but late production examples differed considerably in detail. These were fitted with 110 hp (82 kW)
Clerget 9Z and 130 hp (97 kW) Clerget 9B
rotaries.
Mitsubishi Army Type 甲 1 (Ko 1) Trainer
Japanese designation for licence built Nieuport 81 E.2s. 57 built.[5]
Trainer Type 1
Siamese designation for Nieuport 80 E.2.
Sipowicz 1
Polish experimental aircraft using lifting struts similar to the Wright-Bellanca WB-2.

Operators

 Argentina
 Belgium
  • Belgian Air Force
 Chile
 France
  • Aéronautique Militaire
 Estonia
 Greece
  • Royal Hellenic Navy
 Japan
 Poland
 Portugal
 Romania
 Russian Empire
 Serbia
  • Serbian Air Force
Siam
 United Kingdom
 United States
  • American Expeditionary Force
 Soviet Union
Workers' and Peasants' Air Fleet
Nieuport 12 at the Canada Aviation and Space Museum.

Survivor

A single ex-French Nieuport 12 is on display following an extensive restoration (including reinstalling the original

1918 flu pandemic resulted in it being placed in storage. In the late 1960s the Royal Canadian Air Force
partially converted it into an RFC Beardmore example for display.

Specifications (French-built Nieuport 12 A.2)

Drawing of late production Beardmore-built Nieuport 12 incorporating their modifications

Data from Davilla, 1997, p.369

General characteristics

Performance

  • Maximum speed: 146 km/h (91 mph, 79 kn) at 2,000 m (6,600 ft)
  • Range: 500 km (310 mi, 270 nmi)
  • Endurance: 3 hours
  • Service ceiling: 4,000 m (13,000 ft)
  • Time to altitude: 14 minutes 15 seconds to 2,000 m (6,600 ft)

Armament

  • 1 × .303 in (7.7 mm) Lewis gun on Etévé gun ring in rear cockpit and occasionally a second one on the upper wing

See also

Related development

Related lists

References

Notes

  1. ^ Hartmann, Gérard. "Les Nieuport de la guerre" (PDF). Dossiers historiques et techniques aéronautique française (in French). Retrieved 20 August 2015.
  2. ^ Bruce 1982, p.320.
  3. ^ Bruce 1982, p.323.
  4. ^ Bruce 1982, pp. 323–324.
  5. ^ a b Mikesh and Abe 1990, p. 176.
  6. ^ Hartmann, 2015, p.20

Bibliography