Tu-106 - Specifications
DB-156 build on the basis of the aircraft "105" long-range supersonic bomber Tu-22 with two bypass turbofan engine NK-6. | |
The maximum speed | Flight - 1800-2000 km / h; |
The practical range with 3 tons of bombs |
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Service ceiling over the target
TU-106K) with a thin high-wing | supersonic speed - 16000-17000 m; |
The length of take-off run | 1800-2000 m. |
The range of the aircraft at the rate of the carrier |
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Takeoff thrust | 22000 kg; |
Specific fuel consumption | at takeoff - 1.7 kg / kg. h; |
Specific consumption when drawn 12000 kg, height | 11000 m, the speed of 1400 km / h ~ 1.6 kg / h; |
Motor weight | 3200 kg. |
Tu-106R | |
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Wingspan | 23.6 m; |
Aircraft length | 42.0 m; |
The height of the parking lot | 10.7 m; |
Take-off weight | 100000 kg; |
The maximum flight speed | 2200 km / h; |
Supersonic cruising flight speed | 1800 km / h; |
Subsonic cruising flight speed | 950 km / h; |
Range supersonic cruising speed of 1800 km / h | "14000-17000 m altitude - 4000 km; |
Range subsonic cruise speed of 950 km / h | altitudes 8000-11000 m - 6300 ~ 6500 km; |
Range at low altitudes | 300-500 meters, at a speed of 860 km / h - 3800 km; |
Range on combined profile with a takeoff weight of 110,000 kg overload: | 2000 km, the speed of 950 km / h, the height of 7500-8500 meters, 1,900 km; speed of 1800 km / h, the height of 14600-16000 m, 1800 km; speed of 950 km / h, the height of 12000 m |
Ceiling of in the target area | 18000-19000 m; |
X-22 ASM | |
range of the X-22 | target of the "cruiser" - 400-500 km; |
Area targets - 500-600 km; | |
Minimum convergence of the aircraft carrier with the aim | 300-400 km; |
Starting height of the X-22 | 10000-14000 m; |
Altitude X-22 | 20000-22000 m; |
Flight speed of the X-22 | 2700-3000 km / h; |
Starting weight of the X-22 | 4200-4500 kg; |
Weight of the warhead Kh-22 | 950-1000 kg. |
GKAT and KB-1 at the stage of preliminary design had to work out proposals to increase the start-up range X-22 to 800-1000 km area targets. |
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