Antonov An-180
Antonov An-180 | |
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PICTURE WANTED | |
Type: | Passenger plane |
Design country: | |
Manufacturer: | |
First flight: |
- |
Commissioning: |
- |
Production time: |
- |
Number of pieces: |
0 |
The Antonov An-180 was a project by the Ukrainian aircraft manufacturer Antonow .
development
The design provided for a middle - wing passenger aircraft with swept wings and a turboprop drive. The development started in 1991 was discontinued in 2005. The intended attachment of the Iwtschenko Progress D-27 turboprop engines, each equipped with two counter-rotating propellers , at the ends of pylons below the T-tailplane should be emphasized . Initially, it was planned to mount the engines at the ends of the horizontal stabilizer. The seating was provided in the arrangement 2-2-2.
The first flight was originally supposed to take place in 1995.
Technical specifications
Parameter | Data |
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crew | 2 + 2 cabin |
Passengers | 175 |
length | 43.00 m |
span | 35.60 m |
Hull diameter | 4.30 m |
Wing area | 127 m² |
Max. payload | 18,000 kg |
Empty mass | 42,500 kg |
Max. Takeoff mass | 71,700 kg |
Cruising speed | 800 km / h. |
Service ceiling | 10,100 m |
Engines | two turboprop engines ZMKB Progress Ivchenko Progress D-27 each 10,210 kW (13,882 PS) |