Antonov An-218
Antonov An-218 |
|
Role |
Widebody airliner |
Manufacturer |
Antonov |
Status |
Project is abandoned |
Number built |
0 |
|
The Antonov An-218 was a proposal by the Antonov Design Bureau for a widebody commercial airliner. A twin-engined design, it was intended to carry approximately 350 passengers.
The first flight was initially scheduled for 1994. Due to the severe economical conditions the project was abandoned.
Only a full-scale wooden replica of An-218 was built, but eventually it was taken apart.[1]
Specifications (An-218-100, as designed)
General characteristics
- Crew: 2 (flight deck)
- Capacity: 300/350/400 passengers
- Length: 59.79 m (196 ft 2 in)
- Wingspan: 50 m (164 ft 1 in)
- Height: 15.7 m (51 ft 6 in)
- Wing area: 270 m2 (2,900 sq ft)
- Empty weight: 90,000 kg (198,416 lb)
- Max takeoff weight: 170,000 kg (374,786 lb)
- Powerplant: 2 × Progress D-18T1 high bypass turbofan, 250 kN (57,000 lbf) thrust each
Performance
- Maximum speed: 870 km/h (541 mph; 470 kn)
- Range: 11,500 km (7,146 mi; 6,210 nmi)
See also
- Aircraft of comparable role, configuration and era
References
External links
|
---|
| Airliners | |
---|
| Transports | |
---|
| Reconnaissance and surveillance | |
---|
| Experimental | |
---|
| Gliders | |
---|
| Microlights | |
---|
|
|
---|
| General | |
---|
| Military | |
---|
| Accidents / incidents | |
---|
| Records | |
---|
| Misc. | |
---|
|