Engineering:Grigorovich M-11

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M-11
Grigorovič M-11.jpg
Role Single-seat fighter flying boat
National origin Russia
Manufacturer Shchetinin
Designer Dmitry Pavlovich Grigorovich
First flight 1916
Number built 60+

The Grigorovich M-11 (or Shchetinin M-11) was a Russian single-seat fighter flying boat designed by Dmitry Pavlovich Grigorovich and built by Shchetinin

Design and development

Originally conceived as a two-seater the prototype M-11 was built in 1916 at the Shchetinin factory in Petrograd. The M-11 was a biplane with a 100 hp (75 kW) Gnome Monosoupape rotary engine with a pusher propeller strut mounted below the upper wing. The small number of two-seaters had a poor performance and were only used as trainers, Grigorovich developed a single-seat version powered by a 110 hp (82 kW) Le Rhône engine and fitted with a forward firing machine gun in front of the cockpit. Originally 100 single-seat M-11s had been ordered but this was reduced to 60 as the aircraft had poor handling when landing or alighting on water. The M-11 was operated from snow and ice with twin skis fitted under the forward fuselage and a single ski under the tailplane.

To improve the water handling an improved variant was developed as the M-12 which had a re-designed hull and reduced loaded weight. Although the climb to height was improved the forward speed was 5 mph (8 km/h) less than the M-11 consequentially only a few M-12s were built.

Variants

M-11 (two-seat)
Small numbers built for training use.
M-11 (single-seat)
Production variant, 60 built.
M-12
Improved version.

Operators

 Estonia
 Russia
  • Imperial Russian Navy
 Soviet Union
  • Soviet Naval Aviation

Specifications (M-11 single-seater)

Data from [1]

General characteristics

  • Crew: 1
  • Length: 7.60 m (24 ft 11.25 in)
  • Wingspan: 8.75 m (28 ft 8.5 in)
  • Wing area: 26 m2 (279.87 sq ft)
  • Empty weight: 676 kg (1,490 lb)
  • Gross weight: 926 kg (2,041 lb)
  • Powerplant: 1 × Le Rhône rotary piston , 82 kW (110 hp)

Performance

  • Maximum speed: 148 km/h (92 mph, 80 kn)
  • Endurance: 2 hours 42 minutes

Armament

  • 1 x 7.62mm (0.3 in) Maxim machine-gun

See also

Related lists

References

  1. Orbis 1985, page 2013

Bibliography

  • Gerdessen, Frederik. "Estonian Air Power 1918 – 1945". Air Enthusiast, No. 18, April – July 1982. pp. 61–76. ISSN 0143-5450.
  • Kulikov, Victor (December 1996). "Le fascinante histoire des hydravions de Dimitry Grigorovitch" (in French). Avions: Toute l'aéronautique et son histoire (45): 20–33. ISSN 1243-8650. 
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. 
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.