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Grigorovich I-1

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Grigorovich I-1
RoleFighter
Type of aircraft
National originSoviet Union
ManufacturerGrigorovich Design Bureau
DesignerDmitry Pavlovich Grigorovich
First flightJanuary 1924
StatusPrototype
Number built1
VariantsGrigorovich I-2

TheGrigorovich I-1 was aSovietfighter prototype of the 1920s. It was the first land-based fighter developed by theGrigorovich Design Bureau, who had previously concentrated on water-borne aircraft such as theGrigorovich M-5 of 1914.

Development

[edit]

Initially, design was started on a single-seat fighter byDmitry Pavlovich Grigorovich, to compete with thePolikarpov I-1 biplane. The finished aircraft, finalised in 1924 and produced at Factory No. 1, atKhodinka, nearMoscow, was a single-seat, single-baybiplane of wooden construction, with the forward portion of the fuselage being covered inplywood and the rear having fabric skinning. In development, a major problem was that of engine cooling - various methods were tested including radiators attached to the undercarriage legs, but in the end a radiator suspended beneath the engine was used.

Operational history

[edit]

After an initial flight in January 1924, testing took place in the spring of that year. The I-1 was found to have adequate speed for its purpose but its construction and therefore its flight were unstable, and itsclimb rate was found to be insufficient with repeatedstalls. Therefore, the prototype was abandoned, and Grigorovich refined the design into theGrigorovich I-2 which later entered service in theSoviet Air Force.

Variants

[edit]
Grigorovich I-2
Aerodynamically more refined version of the I-1, entered service in 1926.

Specifications (I-1)

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Data from The Complete Book of Fighters[1]

General characteristics

  • Crew: one
  • Length: 7.32 m (24 ft 0 in)
  • Wingspan: 10.8 m (35 ft 5 in)
  • Wing area: 26.8 m2 (288 sq ft)
  • Airfoil: Göttingen 436[2]
  • Powerplant: 1 ×Liberty L-12 V-12 water-cooled piston engine, 300 kW (400 hp)
  • Propellers: 2-bladed wooden fixed-pitch propeller

Performance

  • Maximum speed: 230 km/h (140 mph, 120 kn)
  • Range: 600 km (370 mi, 320 nmi)
  • Service ceiling: 6,000 m (20,000 ft)

Armament

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

References

[edit]
  1. ^Green, William; Gordon Swanborough.The Complete Book of Fighters. Godalming, UK: Salamander Books. pp. 256–257.
  2. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.
Grigorovich aircraft
Sovietfighter designations, 1923–1940
Fighters (I)
Two-seat fighter (DI)
Multi-seat fighter (MI)
Cannon fighter (IP)
Descriptors
1 Unknown/not assigned
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