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Model: F-4. Gross Mass: 22,517 kg (49,641 lb). Empty Mass: 13,394 kg (29,528 lb). Thrust (vac): 105.578 kN (23,735 lbf). Isp: 2,020 sec. Burn time: 6,000 sec. Propellants: Air/Kerosene. Isp(sl): 1,836 sec. Diameter: 5.03 m (16.50 ft). Span: 11.70 m (38.30 ft). Length: 19.20 m (62.90 ft). Country: USA. No Engines: 2. Motor: J79-17. Status: Retired 1970. Cost $ : 8.000 million. First Flight: 1965. Last Flight: 1966. No Launched: 2. Payload: 5,442 kg (11,997 lb). Release velocity: 650 m/s (2,130 ft/sec). Release altitude: 18 m (58 ft). Release conditions: 2,353 kph at 17.8 km. McDonnell Fighter-cropped delta. Maximum release conditions: 5,442 kg at 2,353 kph at 17,820 m altitude Used on Launch Vehicles: 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. |