Grigorovich I-1
Role Fighter
National origin Soviet Union
Manufacturer Grigorovich Design Bureau
Designer Dmitry Pavlovich Grigorovich
First flight January 1924
Status Prototype
Number built 1
Variants Grigorovich I-2

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

Development

Initially, design was started on a single-seat fighter by Dmitry Pavlovich Grigorovich, to compete with the Polikarpov I-1 biplane. The finished aircraft, finalised in 1924 and produced at Factory No. 1, at Khodinka, near Moscow, was a single-seat, single-bay biplane of wooden construction, with the forward portion of the fuselage being covered in plywood 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

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 its climb rate was found to be insufficient with repeated stalls. Therefore, the prototype was abandoned, and Grigorovich refined the design into the Grigorovich I-2 which later entered service in the Soviet Air Force.

Variants

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

Specifications (I-1)

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

Related development

Aircraft of comparable role, configuration, and era

References

  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. Retrieved 16 April 2019.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.