- First flight1951
- Introduction1954
- StatusRetired
- Number built166
Specifications
01
Crew & dimensions
- Crew
- 1
- Length
- 11.7 m (38.4 ft)
- Wingspan
- 13.1 m
- Height
- 4.26 m
02
Performance
- Maximum speed
- 1,060 km/h
- Range
- 885 km
- Service ceiling
- 15,250 m
03
Powerplant
- Powerplant
- 1 × SNECMA Atar 101D axial flow turbojet ( hp / kW / shp / lbf / 29.4 kN / lbf with afterburner)
04
Armament
- Armament
- Guns: 2× 30 mm DEFA cannon with 150 rounds per gun; Bombs: 900 kg of payload on four external hardpoints, including a variety of bombs or Drop tanks; Rockets: 2× Matra rocket pods with 18× 68 mm SNEB rockets each; Other: Optional 2000 lbs of external ordnance including conventional drop bombs and up to 12 High Explosive (HE) air-to-ground rockets