Mikoyan-Gurevich MiG-110
| RSK MiG-110 | |
|---|---|
| Type: | Multipurpose aircraft |
| Design country: | |
| Manufacturer: | |
| Number of pieces: |
only project |
The Mikoyan-Gurevich MiG-110 ( Russian РСК МиГ-110 ) was a planned Russian passenger / cargo aircraft, the development of which began in 1995, but was never built. It would have been a cantilevered shoulder wing with a double tail girder and a tailgate. The two vertical stabilizers should be connected with a raised horizontal stabilizer. The trapezoidal inverted gull wing initially runs up to the engine nacelles in a negative V position , from the nacelles to the wing tips ending in winglets straight. As drive two were Klimov TW7-117 - propeller turbines provided.
development
The history of the MiG-110 goes back to 1995. Different versions were planned, including a version as a transport aircraft and a variant for a regional airliner with a capacity of 49 passengers. The military transport version could not prevail against the Il-114 and Sukhoi Su-80 in two competitions of the Russian Ministry of Defense in 1999 and 2003 . Even in the later competition, the design of the MiG-110 had no chance against the Antonov An-140 and the Russian authorities' decision to procure the Il-112W instead of the An-140 due to the crisis in the Ukraine. A major disadvantage of the MiG-110 was the tailgate that opened upwards and the relatively short lowerable ramp. Only a 1: 1 mock-up of the MiG-110 was built, a prototype was not built.
Planned versions
- MiG-110N - civil passenger version
- MiG-110NP - paramilitary version
- MiG-110M - combined passenger / cargo version with all-weather and STOL capability. Western engines and avionics were intended for export.
- MiG-110A - Version for joint project and production in Austria.
- MiG-110WT - version for the Russian Air Force.
- MiG-110PR - reconnaissance and rescue version .
Technical specifications
| Parameter | Data MiG-110M |
|---|---|
| crew | 2 |
| Passengers | 49 |
| length | 18.9 m |
| span | 25.0 m |
| height | 5.4 m |
| Wing area | |
| Wing extension | |
| Hold length | 7.4 m |
| Cargo hold width | 2.2 m |
| Cargo space height | 2.2 m |
| payload | 5,500 kg |
| Empty mass | |
| Max. Takeoff mass | 15,300 kg |
| Cruising speed | 500 km / h |
| Top speed | |
| Cruising altitude | 11,000 m |
| Range | 4,050 km |
| Engines | 2 × Turboprop Klimow TW7-117 with 2,500 PS (1,839 kW) each |
Comparable types
literature
- Jefim Gordon , Sergei Komissarow: Unflown Wings: Soviet / Russian unrealized aircraft projects 1925-2010 . Ian Allen Publishing, 2013, ISBN 978-1-906537-34-0 .
- Piotr Butowski, Jay Miller: OKB MiG: A History of the Design Bureau and its Aircraft . Specialty Pr Pub & Wholesalers, Leicester 2000, ISBN 0-904597-80-6 .
- George. E. Slagley: A Century of Aviation: Worldwide Commercial and Military . Strategic Book, Durham 2011, ISBN 978-1-61204-093-6 , pp. 123 .
Web links
- MiG-110. toad-design.com, accessed on November 29, 2018 (English).
Individual evidence
- ↑ a b c d e Mikoyan braves finance snags for MiG-110 work. www.flightglobal.com, June 9, 1999, accessed November 29, 2018 .
- ↑ IL-112 multi-purpose transport ( Memento of the original dated August 6, 2018 in the Internet Archive ) Info: The archive link was inserted automatically and has not yet been checked. Please check the original and archive link according to the instructions and then remove this notice. on kamov.net (English)
- ↑ Crack illustration with technical data , airpower.at, accessed on November 29, 2018
- ↑ MiG-110 production in Austria is becoming more and more likely. In: airpower.at. June 18, 2000, accessed November 29, 2018 .
