Grigorovich I-2
The Grigorovich I-2 was a biplane fighter aircraft of the Soviet Union, the first indigenous fighter to enter service in substantial numbers. Developed from the Grigorovich I-1, it first flew on 4 November 1924, piloted by A.I. Zhukov. The M-5 engine was a Soviet copy of the Liberty L-12.
Production of the redesigned I-2bis was 211 aircraft. Production was performed by Aviation Repair Plant No.3 in Smolensk.
Operators
- Soviet Union
Specifications (I-2bis)
General characteristics
- Crew: One, pilot
- Length: 7.32 m (24 ft 0 in)
- Wingspan: 10.80 m (35 ft 5 in)
- Height: 3.00 m (9 ft 10 in)
- Wing area: 23.4 m² (252 ft²)
- Empty weight: 1,152 kg (2,540 lb)
- Loaded weight: 1,575 kg (3,472 lb)
- Powerplant: 1 × M-5 water-cooled 45-degree V12 engine, 298 kW (400 hp)
Performance
Armament
See also
- Related development
- Related lists
External links
Soviet fighter designations |
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| I (Istrebítel - "Fighter") | |
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| DI (Dvukhmestnyi Istrebitel - "Two-seat Fighter") | |
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| MI (Mnogomestnyi Istebitel - Multi seat fighter | |
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