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| MIRAGE F1 (DASSAULT-BREGUET) - General Characteristics. |
| Country of Origin | France |
|
Builder team : |
Dassault Aviation, SNECMA, Thomson-CSF |
| Role |
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|
First flight : |
November 1981 |
|
In-service in French Air Force : |
1983 |
| Similar Aircraft | |
| Crew | |
| Length | 49 ft (14.94 m) 15.33 m |
| Span | 27 ft, 7 in (8.4 m) |
|
Height : |
4.50 m |
|
Weight |
8.1 t empty |
|
Power plant / Thrust : |
SNECMA Atar 9K50 jet engine / 4.7 t and 6.8 t with afterburner |
| Ceiling | 52,000 ft [20,000 meters ?] |
|
Maximum speed : |
Mach 2.2 |
| Cruise range | 1160 nm |
| In-Flight Refueling | Y |
| Internal Fuel | 3435 kg |
|
Fuel capacity : |
4,100 l internal / 6,400 l maximal / In-flight refuelling |
| Payload | 6300 kg |
| Sensors | Cyrano IVM radar (-200 has IWMR), RWR |
| Drop Tanks | 1160 L drop tank with 927kg of fuel for 157nm of
range 2300 l drop tank with 1837kg of fuel for 310nm of range |
| Armament | |
|
Special equipment : |
Radar Thomson-CSF Cyrano IV-MR (air-to-air, air-to-ground), inertial navigation system, panoramic camera Omera 40, vertical camera Omera 33, IR thermographic captor Super Cyclope, lateral radar Raphael, electromagnetic emissions detector Astac, photographic pod RP35P, Desire digital video recce pod, electronic counter measures |
|
NATO interoperability : |
In-flight refuelling by NATO aircraft, armament and ammunitions in accordance with NATO standards |
| User Country |
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Number of units produced : |
740 (all types of Mirage F1 included) |
|
French Air Force inventory : |
40 aircraft in 2 squadrons |
keywords: aircraft, fighter
