Israel Aircraft Industries (IAI) - Israel
Manufacturer(s)
Argentina; Israel; South Africa
Operators
1972
Service Year
Israel
National Origin
1
Crew
61
Units
AIR-TO-AIR COMBAT
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
CLOSE-AIR SUPPORT
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.
51.3 ft
(15.65 meters)
Length
27.0 ft
(8.22 meters)
Width/Span
14.8 ft
(4.50 meters)
Height
14,551 lb
(6,600 kilograms)
Empty Weight
29,762 lb
(13,500 kilograms)
Maximum Take-Off Weight
+15,212 lb
(+6,900 kg)
Weight Difference
1 x SNECMA Atar 09C turbojet engine developing 13,688lb thrust with afterburner (9,435lb dry).
Propulsion
1,460 mph
(2,350 kph | 1,269 knots)
Max Speed
58,005 ft
(17,680 m | 11 miles)
Ceiling
808 miles
(1,300 km | 702 nm)
Range
16,400 ft/min
(4,999 m/min)
Rate-of-Climb
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
STANDARD:
2 x 30mm DEFA 552 internal cannons
OPTIONAL:
Up to 8,800 lb of conventional ordnance across five external hardpoints.