| Mirage 4A |
home
topic index |
|
Model: Mirage 4A. Gross Mass: 26,213 kg (57,789 lb). Empty Mass: 14,494 kg (31,953 lb). Thrust (vac): 96.046 kN (21,592 lbf). Isp: 2,020 sec. Burn time: 15,000 sec. Propellants: Air/Kerosene. Isp(sl): 1,836 sec. Diameter: 5.64 m (18.50 ft). Span: 11.85 m (38.87 ft). Length: 23.44 m (76.90 ft). Country: France. No Engines: 2. Motor: Atar 9K. Status: Out of Production. Payload: 7,256 kg (15,996 lb). Release velocity: 650 m/s (2,130 ft/sec). Release conditions: 2,345 kph at 20 km. Dassault Bomber-delta wing. Maximum release conditions: Belly mounted, 7,256 kg at 2,345 kph at 20,000 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. |