The genesis of Mirage III goes back to 1951, when a team of DASSAULT's engineering and design department works on an interceptor equipped with a delta wing. Learning the lessons from the Korean War, the Armée de l'Air emitted, during the year 1953, a programs concerning a fighter able to carry all-weather armaments to a 18000 m altitude in less than 6 mn. Twin-jet aircraft prototypes MD.550 Mystère Delta (2 Armstrong-Siddeley Viper turbojets of 795 kg thrust and one SEPR.66 booster of 1500 kg thrust) and Mirage I (2 MD30R turbojet of 1000 kg thrust with afterburning) don't allow to reach the desired performance by the Armée de l'Air de l'Air, DASSAULT company decide then to make evolve the delta formula to a new single engined aircraft (SNECMA Atar 9 of 4500 kg thrust with afterburning) and of which the fuselage answer with law of surface (the famous size of wasp). This plane, the Mirage III 001, first flew on November 17, 1956 by Roland Glavany and reached Mach 1.24 during the 4th flight, December 3. The aircraft does not manage nevertheless to reach Mach 2 (Mach 1,89 with booster on
October 2, 1957, during the 84th flight). It is in particular thanks to the adoption of central mobile conical cores in the air intake (mice) that Roland Glavany reaches Mach 2, for the 1st time in Western Europe, on the Mirage III A01, October 24, 1958. Thereafter, from many versions rose from the Mirage III, of which the 1st Mirage III C (C for Chasse and Cyrano, the radar).| Technical features | ||
| Wingspan | 8,22 m | ![]() |
| Length | 14,75 m | |
| Height | 4,25 m | |
| Wingspan | 34,85 m2 | |
| Empty weight | 5922 kg | |
| Max weight | 11700 kg | |
| Max speed | Mach 2,15 at 11000 m | |
| Max Ceiling | 24600 m | |
| Ceiling | 18000 m | |
| Climb | 18000 m in 6,16 min with booster | |
| Range | 1500 km at Mach 0.85 and 12000 m | |
| Turbojet | 1 SNECMA Atar 9B-3 4250 kg thrust 6000 kg with afterburning + SEPR 841 booster of 1500 kg thrust. | |
| Basic armament | 2 x 30 mm DEFA 552 Cannons 125 shells each | |
| CAEA's specimen |
Mirage III C s/n 2 was first flown on December 13, 1960, by Jean Coureau, then will be delivered to the Armée de l'Air on January 20, 1961, within the CEAM where it will fly until February 12, 1965. Victim of an accident when landing in Mont-de-Marsan October 30, 1961, due to a right gear problem, the # 2 will turn over to Mérignac to be repaired there. After the CEAM it is affected at the CEV until January 28, 1991, where it will be specialized in the AS.37 missile test flights. It is finally returned to the Armée de l'Air, at the ETSAA.308 in Cazaux, before joining the CAEA in September 1998.Visible in the hangar |
Contact : Gérard and Olivier Weber
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![]() Mirage III B |