Mikoyan MiG-110
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The Mikoyan-Gurevich MiG-110 (МиГ-110 in Russian language) is a Russian passenger/cargo aircraft that began development in 1995 but has not yet flown. It is of pod-and-boom configuration, to be powered by twin turboprop engines.
[edit] 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.
[edit] Specifications (MiG-110M, as designed)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 2
- Capacity:
- Passengers: 49
- Cargo: 5,500 kg (12,000 lb)
- Length: 18.9 m (62 ft 0 in)
- Wingspan: 25.0 m (82 ft 0 in)
- Height: 5.4 m (18 ft)
- Wing area: m² (ft²)
- Empty weight: kg (lb)
- Loaded weight: kg (lb)
- Max takeoff weight: 18,000 kg (40,000 lb)
- Powerplant: 2× Pratt & Whitney Canada PW127C turboprops, 1,846 kW (2,475 hp) each
Performance
- Maximum speed: 500 km/h (270 kn, 308 mph)
- Range: 3,710 km (2,000 nmi, 2,310 mi)
- Service ceiling m (ft)
- Rate of climb: m/s (ft/min)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
[edit] See also
Related lists
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