| Manufacturer |
Tupolev |
Ilyushin |
| Description |
The Tupolev Tu-95LAL experimental aircraft () which flew from 1961 to 1965 was a modified Tupolev Tu-95 Soviet bomber aircraft, analogous to the United States' earlier Convair NB-36H. |
The Ilyushin Il-76 (; NATO reporting name: Candid) is a multi-purpose, fixed-wing, four-engine turbofan strategic airlifter designed by the Soviet Union's Ilyushin design bureau as a commercial freighter in 1967, to replace the Antonov An-12. |
| ICAO Code |
|
IL76 |
| First Flight |
1961-01-01 |
|
| Designer |
Tupolev |
Ilyushin |
| Type |
Experimental nuclear aircraft |
Strategic and tactical airlifter |
| Length (m) |
46.2 |
46.6 |
| Height (m) |
12.12 |
14.42 |
| Cockpit Crew |
|
5 |
| Cruise Speed (km/h) |
750 |
750 |
| Max Ceiling (m) |
|
12200 |
| Armament |
|
2 × 23 mm cannon in radar-directed manned turret at base of tail; Some military models have four hardpoints under each outer wing capable of supporting 500 kg bombs. |
| Capacity Description |
|
Il-76M 42000 kg; Il-76MD 48000 kg; Il-76MD-90A 60000 kg |
| Endurance (h) |
6.4 |
|
| National Origin |
|
Soviet Union |
| Number Built |
1 |
981 |
| Powerplant Description |
4 × Kuznetsov NK-12M turboprop engines |
4 × Aviadvigatel PS-90A-76 turbofans, 156.9 kN thrust each |
| Primary Users |
|
Soviet Air Forces (historical), Russian Aerospace Forces , People's Liberation Army Air Force , Indian Air Force |
| Status |
|
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Tupolev_Tu-95LAL |
en.wikipedia.org/wiki/Ilyushin_Il-76 |
| Flat Wing Span (m) |
50.1 |
50.5 |
| Flat Wing Area (m²) |
310 |
300 |
| Wake Category |
|
H |
| Aircraft Engine |
|
Aviadvigatel PS-90 |
| Number of Engines |
4 |
4 |