Mikoyan MiG-110

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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.

Proposed Variants[edit]

  • 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)[edit]

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

  • Cruising 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 (36,089 ft)

See also[edit]