| F-106 |
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Model: F-106. Gross Mass: 15,173 kg (33,450 lb). Empty Mass: 10,901 kg (24,032 lb). Thrust (vac): 71.598 kN (16,096 lbf). Isp: 1,800 sec. Burn time: 6,000 sec. Propellants: Air/Kerosene. Isp(sl): 1,636 sec. Diameter: 6.21 m (20.37 ft). Span: 11.70 m (38.30 ft). Length: 21.55 m (70.70 ft). Country: USA. No Engines: 1. Motor: J75-17. Status: Out of Production. Cost $ : 12.710 million. Payload: 1,957 kg (4,314 lb). Release velocity: 595 m/s (1,952 ft/sec). Release altitude: 16 m (53 ft). Release conditions: 2,141 kph at 16.1 km. Convair Interceptor-delta wing. Maximum release conditions: Weapons bay mounted, 1,957 kg at 2,141 kph at 16,067 m altitude Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |