| Manufacturer |
Tupolev |
Tupolev |
| Description |
The Tupolev Tu-107 was a prototype Soviet military transport aircraft developed from the Tupolev Tu-104. |
The Tupolev Tu-104 (NATO reporting name: Camel) is a medium-range, narrow-body, twin turbojet-powered Soviet airliner. |
| First Flight |
1958-01-01 |
1955-06-17 |
| Entry Into service |
|
1956-09-15 |
| Production End |
|
1960-01-01 |
| Service End |
|
1981-01-01 |
| Designer |
Tupolev |
Andrei Tupolev |
| Type |
Military jet transport aircraft |
Narrow-body jetliner |
| Length (m) |
38.58 |
40.06 |
| Height (m) |
11.53 |
11.9 |
| Cockpit Crew |
6 |
7 |
| Max Seating |
70 |
115 |
| Max Speed (km/h) |
950 |
950 |
| Cruise Speed (km/h) |
775 |
|
| Max Ceiling (m) |
11750 |
12000 |
| Rate of Climb (m/s) |
|
10 |
| Armament |
; 2 x 23mm Afanasev Makarov AM-23 cannon in a DK-7T powered tail turret aimed via a TSP-1 television sighting system and PRS-2 Argon-2 gun ranging radar |
|
| Capacity Description |
70 paratroops or 10,000 kg – 15,000 kg payload |
50–115 passengers |
| National Origin |
Soviet Union |
|
| Number Built |
1 |
201 |
| Powerplant Description |
2 × Mikulin RD-3M-500 Axial flow turbojet engines, 93.2 kN thrust each |
2 × Mikulin AM-3M-500 turbojet engines |
| Primary Users |
|
Aeroflot, ČSA |
| Status |
|
Retired |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Tupolev_Tu-107 |
en.wikipedia.org/wiki/Tupolev_Tu-104 |
| Flat Wing Span (m) |
34.54 |
34.54 |
| Flat Wing Area (m²) |
174.48 |
183 |
| Number of Engines |
2 |
2 |