Tu-160

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Tu-160

Tu-160SK with Burlak

Mach 2 rocket launch aircraft. Tupolev Bomber-variable geometry. Maximum release conditions: Belly-mounted, 9,977 kg at 2,451 kph at 18,292 m altitude

Status: Development ended 1992. Payload: 28,000 kg (61,000 lb). Thrust: 533.67 kN (119,974 lbf). Gross mass: 205,442 kg (452,922 lb). Unfuelled mass: 99,773 kg (219,961 lb). Specific impulse: 1,980 s. Specific impulse sea level: 1,800 s. Burn time: 58,000 s. Height: 53.35 m (175.03 ft). Diameter: 13.71 m (44.98 ft). Span: 53.96 m (177.03 ft). Location: 500.

No Engines: 4. Release velocity: 500 m/s (1,640 ft/sec). Release altitude: 14 m (44 ft). Release angle: 0 deg.

Country: Russia. Engines: NK-231. Launch Vehicles: Burlak. Propellants: Air/Kerosene.

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