Harman Patil (Editor)

Tupolev I 12

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Top speed
  
300 km/h

Length
  
9.52 m

Designer
  
Andrei Tupolev

Wingspan
  
16 m

Manufacturer
  
Tupolev

Tupolev I-12 httpsuploadwikimediaorgwikipediaen669Tup

The Tupolev I-12 (also known as the ANT-23) was a prototype Soviet fighter aircraft that never reached production. The I-12 was of unconventional design with twin booms made of water pipes containing recoilless rifles and two engines in a push-pull configuration. The aircraft first flew in 1931 but did not enter production due to disappointing performance and operational difficulties such as the inability for the pilot to escape the aircraft without hitting the propeller arc behind him. The second prototype from Tupolev (designated ANT-23bis) was never completed.

Specifications

Data from Shavrov 1985

General characteristics

  • Crew: one
  • Length: 9.5 m (31 ft 2 in)
  • Wingspan: 15.6 m (51 ft 2 in)
  • Height: ()
  • Wing area: 30 m² (322.9 ft²)
  • Loaded weight: 2,400 kg (5,291 lb)
  • Powerplant: 2 × Gnome-Rhône 9Ak radial engines, 392 kW (525 hp) each
  • Performance

  • Maximum speed: 300 km/h (162 kn, 186 mph)
  • Wing loading: 80 kg/m² (16 lb/ft²)
  • Power/mass: 326 W/kg (0.2 hp/lb)
  • Armament

  • 2 × 76.2 mm (3 in) APK-4 recoilless rifles
  • References

    Tupolev I-12 Wikipedia