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F-4
Mach 2 rocket launch aircraft. McDonnell Fighter-cropped delta. Maximum release conditions: 5,442 kg at 2,353 kph at 17,820 m altitude

Status: Retired 1970. Payload: 5,442 kg (11,997 lb). Thrust: 105.58 kN (23,735 lbf). Gross mass: 22,517 kg (49,641 lb). Unfuelled mass: 13,394 kg (29,528 lb). Specific impulse: 2,020 s. Specific impulse sea level: 1,836 s. Burn time: 6,000 s. Height: 19.20 m (62.90 ft). Diameter: 5.03 m (16.50 ft). Span: 11.70 m (38.30 ft). Location: 650.

Cost $ : 8.000 million. No Engines: 2. Release velocity: 650 m/s (2,130 ft/sec). Release altitude: 18 m (58 ft). Release conditions: 2,353 kph at 17.8 km.

Country: USA. Engines: J79-17. Launch Vehicles: Sparoair III, ALARR. Propellants: Air/Kerosene. More at: 11045.



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