Mikoyan MiG-110

From Wikipedia, the free encyclopedia

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)

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 PW-127C turboprops, 1,846 kW (2,475 hp) each

Performance

• Maximum speed: km/h (kt, mph)
• Range: 3,710 km (2,000 nm, 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] Related content

 

 

 

Related lists

• List of airliners