Samiksha Jaiswal (Editor)

Mikoyan MiG 110

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Top speed
  
500 km/h

Length
  
18 m

Wingspan
  
22 m

Mikoyan MiG-110 httpsuploadwikimediaorgwikipediavithumba

The Mikoyan-Gurevich MiG-110 (Russian: МиГ-110) was a proposed Russian passenger/cargo aircraft that began development in 1995 but was not built. It would have been a high-mounted cantilever monoplane with a pod-and-boom configuration with a beaver tail rear fuselage, to be powered by two Klimov TV7-117 turboprop engines.

Contents

Proposed Variants

  • MiG-110N – dedicated passenger version
  • MiG-110NP – paramilitary version
  • MiG-110M – combination passenger/freight version with all-weather and STOL capability
  • MiG-110A – version for joint project to produce in Austria.

    • The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

    Specifications (MiG-110M, as designed)

    General characteristics

  • Crew: 2
  • Capacity:
  • Passengers: 49
  • Cargo: 5,500 kg (12,000 lb)
  • Length: 18.5 m (60 ft 8 in)
  • Wingspan: 22.12 m (72 ft 7 in)
  • Max takeoff weight: 15,300 kg (33,731 lb)
  • Powerplant: 2 × Klimov TV7-117 turboprop engines, 1,864 kW (2,500 hp) each

    • Performance

  • Cruise speed: 500 km/h (311 mph; 270 kn)
  • Range: 4,050 km (2,517 mi; 2,187 nmi) with full fuel
  • Service ceiling: 11,000 m (36,000 ft)

    • References

    Mikoyan MiG-110 Wikipedia
    (Text) CC BY-SA


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