Mikoyan MiG-110

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

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

This page contains text from Wikipedia, the Free Encyclopedia - https://wn.com/Mikoyan_MiG-110

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Mikoyan MiG-110

Proposed Variants

Specifications (MiG-110M, as designed)

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