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Initial Operational Capability (IOC):
Also Known As: C-14, Mirage F1A, Mirage F1B, Mirage F1C, Mirage F1CR, Mirage F1CT, Mirage F1D and Mirage F1E
Parent System: Mirage F-1
Initial Operational Capability (IOC): 1973
Total Production: 740
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Description: Mirage F1 is a light single-engine multi-role fighter aircraft developed by Dassault as a successor for Mirage III. It is powered by an Atar 9K-50 turbofan engine rated at 15,800-lb of thrust with afterburning allowing for March 2.2 top speed. It was equipped with upgraded Cyrano IV radar. Mirage F1 was ordered by the French Air Force with deliveries stating in 1973. Over 10 international air forces also ordered this aircraft type. Iran obtained its F1s from Iraqi Air Force which flew to Iran to get shelter during the Gulf War in 1991. Overall, Mirage F1 is suitable for air-to-air and air-to-surface roles.
F1B and F1D are two seat variants. F1C was the standard model in the French Air Force in the early 1980s. Mirage F1CT and F1CR are upgraded aircraft for air-to-ground and reconnaissance roles. French Air Force plans call for Mirage F1s to be replaced by far more capable Rafale C/Bs before 2015. F1s operated by international air forces are being upgraded or retired following the availability of more capable multi-role aircraft such as Rafale, Typhoon, F-16, Gripen etc.
Mirage F1 Specifications
Number of Engines: 1
Height: 4.50 meter (14.8 foot)
Length: 15.3 meter (50 foot)
Main Gun Caliber: 30 millimeter
Wingspan: 8.40 meter (27.6 foot)
Ceiling: 17,000 meter (55,774 foot)
Max Range: 2,150 kilometer (1,161 nautical mile)
Top Speed at High Altitude: 731 mps (2,632 kph)
Max Takeoff Thrust: 15,800 pound (7,167 kilogram)
Max Takeoff Weight: 15,200 kilogram (33,510 pound)
Payload: 6,300 kilogram (13,889 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
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Mirage F1 News
There are 2 news between
24 Sep 2004 and 23 Feb 2012
Operators & Related Equipment
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