Tu-160
Tu-160SK with Burlak
Gross Mass: 205,442 kg (452,922 lb). Empty Mass: 99,773 kg (219,961 lb). Thrust (vac): 533.670 kN (119,974 lbf). Isp: 1,980 sec. Burn time: 58,000 sec. Propellants: Air/Kerosene. Isp(sl): 1,800 sec. Diameter: 13.71 m (44.98 ft). Span: 53.96 m (177.03 ft). Length: 53.35 m (175.03 ft). Country: USSR. No Engines: 4. Engine: NK-231. Status: Development ended 1992. Payload: 28,000 kg (61,000 lb). Release velocity: 500 m/s (1,640 ft/sec). Release altitude: 14 m (44 ft). Release angle: 0 deg.

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

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