| Manufacturer |
Tupolev |
Antonov |
| Description |
The Tupolev Tu-104 (NATO reporting name: Camel) is a medium-range, narrow-body, twin turbojet-powered Soviet airliner. |
The Antonov An-180 was a Ukrainian design for a twin-aisle medium-range propfan airliner. |
| First Flight |
1955-06-17 |
|
| Entry Into service |
1956-09-15 |
|
| Production End |
1960-01-01 |
|
| Service End |
1981-01-01 |
|
| Designer |
Andrei Tupolev |
Antonov |
| Type |
Narrow-body jetliner |
|
| Length (m) |
40.06 |
40.9 |
| Height (m) |
11.9 |
11.148 |
| Cockpit Crew |
7 |
|
| Max Seating |
115 |
|
| Max Speed (km/h) |
950 |
|
| Cruise Speed (km/h) |
|
800 |
| Max Ceiling (m) |
12000 |
10100 |
| Rate of Climb (m/s) |
10 |
|
| Capacity Description |
50–115 passengers |
163 |
| National Origin |
|
Soviet Union |
| Number Built |
201 |
0 |
| Powerplant Description |
2 × Mikulin AM-3M-500 turbojet engines |
2 × Ivchenko Progress D-27 propfan, 10305 kW (13819 hp) each |
| Primary Users |
Aeroflot, ČSA |
|
| Status |
Retired |
Canceled |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Tupolev_Tu-104 |
en.wikipedia.org/wiki/Antonov_An-180 |
| Flat Wing Span (m) |
34.54 |
35.83 |
| Flat Wing Area (m²) |
183 |
|
| Aircraft Engine |
|
Progress D-27 |
| Number of Engines |
2 |
2 |