Mikoyan MiG-110
Type: Twin turboprop multi-purpose transport.
Program: Announced during 1993; shown in model form at MosAeroshow 1993; development received government approval January 1994.
Design features: High-wing monoplane; anhedral center section between twin booms carrying engines at front and twin fins at the rear; horizontal tail surfaces between fin tips; retractable tricycle landing gear; twin wheels on each unit; mainwheels retract into booms to rear of engines; fuselage pod slung from center-section, with beaver-tail rear loading ramp.
Cabin can be equipped for passenger, combined cargo/passenger, or cargo operations.
Flying controls: Conventional ailerons, elevator, and twin rudders.
Power plant: Two 1,838 kW (2,465 shp) Klimov TV7-117SV turboprops; six-blade propellers.
Accommodation: Seats for 35 passengers; or provisions for 15 passengers and 3,500 kg of freight, or 5,000 kg (11,025 lb) freight.
Dimensions external
Wing span: 22.12 m (72 ft 7 in)
Length overall: 18.295 m (60 ft .25 in)
Height overall: 5.395 m (17 ft 8 in)
Dimensions internal
Cargo cabin length: 7.40 m (24 ft 3.5 in)
Cargo cabin max width: 2.20 m (7 ft 2.5 in)
Cargo cabin max height: 2.20 m (7 ft 2.5 in)
Weights and loadings
Max T-O weight: 15,300 kg (33,730 lb)
Performance (estimated)
Nominal cruising speed at 11,000 m (36,000 ft): 270 knots (500 km/h; 310 mph)
Range with max fuel: 2,185 nm (4,050 km; 2,515 miles)
Source: Lambert, Mark ed.
Jane's All the World's Aircraft 1994-1995 Jane's Information Group Ltd. 1994 p. 334.
Model of Mikoyan MiG-110. Note straight wing and absence of winglets.
Source:
http://www.umt.fme.vutbr.cz/~ruja/modely/podklady.htm