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F-106
Mach 2 rocket launch aircraft. Convair Interceptor-delta wing. Maximum release conditions: Weapons bay mounted, 1,957 kg at 2,141 kph at 16,067 m altitude

Status: Out of Production. Payload: 1,957 kg (4,314 lb). Thrust: 71.60 kN (16,096 lbf). Gross mass: 15,173 kg (33,450 lb). Unfuelled mass: 10,901 kg (24,032 lb). Specific impulse: 1,800 s. Specific impulse sea level: 1,636 s. Burn time: 6,000 s. Height: 21.55 m (70.70 ft). Diameter: 6.21 m (20.37 ft). Span: 11.70 m (38.30 ft). Location: 595.

Cost $ : 12.710 million. Release velocity: 595 m/s (1,952 ft/sec). Release altitude: 16 m (53 ft). Release conditions: 2,141 kph at 16.1 km.

Country: USA. Engines: J75-17. Propellants: Air/Kerosene. More at: 9659.



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