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.
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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
- 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
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