Antonov An-180
| Antonov An-180 | |
|---|---|
| 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 |
|---|---|
| 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) |