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 beavertail rear fuselage, to be powered by two Klimov TV7-117 turboprop engines.[1]
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Transcription
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, for production 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)
Data from[citation needed]
General characteristics
- Crew: 2
- Capacity: 49 pax / 5,500 kg (12,125 lb) payload
- 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
- Propellers: 6-bladed constant-speed propellers
Performance
- Cruise speed: 500 km/h (310 mph, 270 kn)
- Range: 4,050 km (2,520 mi, 2,190 nmi) with full fuel
- Service ceiling: 11,000 m (36,000 ft)
See also
References
- ^ Slagley, George E. (2011). A century of aviation: worldwide commercial and military. Durham: Strategic Book Group. p. 123. ISBN 9781612040936.
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This page was last edited on 3 February 2024, at 01:32