- First flight1956
- Introduction1961
- StatusRetired
- Number built1,422
Specifications
01
Crew & dimensions
- Crew
- 1
- Length
- 15.03 m
- Wingspan
- 8.22 m
- Height
- 4.5 m
02
Performance
- Maximum speed
- 2,350 km/h, Mach 2.2
- Range
- 1,200 km (combat range)
- Service ceiling
- 17,000 m
03
Powerplant
- Powerplant
- 1 × SNECMA Atar 09C afterburning turbojet engine (41.97 kN) + 1 × SEPR 841 liquid-fuelled rocket engine (14.7 kN)
04
Armament
- Armament
- Guns: 2 × 30 mm DEFA 552 cannon with 125 rounds per gun; Bombs: 4000 kg of payload on five external hardpoints, including a variety of bombs, reconnaissance pods or Drop tanks; French Air Force IIIEs through to 1991 were equipped to carry the AN-52 nuclear bomb.; Rockets: 2 × Matra JL-100 drop tank/rocket pack, each with 19× 68 mm SNEB rockets and 250 L of fuel; Missiles: 2 × AIM-9B Sidewinder Air to Air missiles (AAM) or, 2 × Matra R.550 Magic AAMs plus 1× Matra R.530 AAM