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The first example of the Mirage II C flew on 9 October 1960 .It was the first production series to be built. The Mirage III C was a single-seat interceptor powered by Atar 09B-3 turbojet Armed with two 125-round DEFA 30-mm cannon, and it was also equipped with five wing pylons .As a interceptor, the aircraft had a whole series of air-to-air missile (Matra R-511 or R-530, Sidewinders) when they used in the ground attack role, which were replaced by air-to ground missiles (AS.20 ,AS.30) or JL100R rocket launchers. The mirage III C had a rather successful export career, being used by Switzerland, Israel and South Africa.
Wingspan: 8.22 m
Length: 14.73 m
Wing Area: 34.85 m2
Power plant: 1 SNECMA "Atar" 09 B-3 jet.
Empty weight: 5922 kg
Armament: Two 125-round DEFA 552 30 mm cannon
range : 2500km