| Manufacturer |
Airbus |
Tupolev |
| Family |
A320 |
|
| Model |
A321 |
|
| Description |
|
The Tupolev Tu-104 (NATO reporting name: Camel) is a medium-range, narrow-body, twin turbojet-powered Soviet 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 |
| Type |
|
Narrow-body jetliner |
| Length (m) |
44.51 |
40.06 |
| Height (m) |
11.76 |
11.9 |
| Cockpit Crew |
2 |
7 |
| Max Seating |
236 |
115 |
| One Class Typical Seating |
199 |
|
| Two Class Typical Seating |
185 |
|
| Cargo Volume (m³) |
51.7 |
|
| Max Speed (km/h) |
|
950 |
| Max Ceiling (m) |
|
12000 |
| Rate of Climb (m/s) |
|
10 |
| Capacity Description |
|
50–115 passengers |
| Number Built |
|
201 |
| Powerplant Description |
|
2 × Mikulin AM-3M-500 turbojet engines |
| Primary Users |
|
Aeroflot, ČSA |
| Status |
|
Retired |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Airbus_A321 |
en.wikipedia.org/wiki/Tupolev_Tu-104 |
| Flat Wing Span (m) |
35.8 |
34.54 |
| Flat Wing Area (m²) |
128 |
183 |
| Wing Sweepback (°) |
25 |
|
| Fuselage Diameter (m) |
3.95 |
|
| Aircraft Engine |
CFM56-5B2/P |
|
| Number of Engines |
2 |
2 |