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Mirage 4A
Mach 2 rocket launch aircraft. Dassault Bomber-delta wing. Maximum release conditions: Belly mounted, 7,256 kg at 2,345 kph at 20,000 m altitude

Status: Out of Production. Payload: 7,256 kg (15,996 lb). Thrust: 96.05 kN (21,592 lbf). Gross mass: 26,213 kg (57,789 lb). Unfuelled mass: 14,494 kg (31,953 lb). Specific impulse: 2,020 s. Specific impulse sea level: 1,836 s. Burn time: 15,000 s. Height: 23.44 m (76.90 ft). Diameter: 5.64 m (18.50 ft). Span: 11.85 m (38.87 ft). Location: 650.

No Engines: 2. Release velocity: 650 m/s (2,130 ft/sec). Release conditions: 2,345 kph at 20 km.



Country: France. Engines: Atar 9K. Propellants: Air/Kerosene.

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