Credit
Carlos Menendez San Juan · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AMX · Length
Single source13.23 m (43 ft 5 in)[source]
MiG-17F · Length
Single sourceConfiguration
| Specification | AMX International AMX | Mikoyan-Gurevich MiG-17 |
|---|---|---|
| Type | Ground-attack aircraft[source] | Fighter aircraft[source] |
| National origin | Italy / Brazil[source] | Soviet Union[source] |
| Manufacturer | AMX International[source] | Mikoyan-Gurevich[source] |
| Status | Active service[source] | In limited service |
11.264 m (36 ft 11 in)[source]
Empty; AMX · Empty weight
Single sourceGross; AMX · Gross weight
Single sourceMaximum take-off; AMX · Max takeoff weight
Single source6,700 kg (14,771 lb)[source]
10,750 kg (23,700 lb)[source]
13,000 kg (28,660 lb)[source]
Empty; MiG-17F · Empty weight
Single sourceGross; MiG-17F · Gross weight
Single sourceFerry; AMX · Ferry range
Single source3,336 km (2,073 mi, 1,801 nmi)[source]
MiG-17F · at 12,000 m (39,000 ft) with 2 × 400 L (110 US gal; 88 imp gal) drop-tanks
Single source2,020 km (1,260 mi, 1,090 nmi) at 12,000 m (39,000 ft) with 2 × 400 L (110 US gal; 88 imp gal) drop-tanks[source]
AMX · hi-lo-hi profile, with 900 kg (1,984 lb) of external stores
Single source889 km (552 mi, 480 nmi) hi-lo-hi profile, with 900 kg (1,984 lb) of external stores[source]
AMX · 1 × Rolls-Royce Spey 807 turbofan engine thrust
Single source1 × Rolls-Royce Spey 807 turbofan engine, 49.1 kN (11,000 lbf) thrust[source]
MiG-17F · 1 × Klimov VK-1F afterburning centrifugal-flow turbojet engine thrust dry
Single sourceMiG-17F · with afterburner
Single source1 × Klimov VK-1F afterburning centrifugal-flow turbojet engine , 26.5 kN (6,000 lbf) thrust dry, 33.8 kN (7,600 lbf) with afterburner[source]
AMX · Endurance
Single source4 hours, 15 minutes[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Italian Air Force (historical) Brazilian Air Force[source] | Soviet Air Forces (historical) People's Liberation Army Air Force (historical) Polish Air Force (historical) Vietnam People's Air Force (historical)[source] |
|---|
| Number built | 230[source] | 10,649 including Polish, Czechoslovak and Chinese variants[source] |
|---|
| Manufactured | 1986–1999[source] | — |
|---|
| Introduction date | 1989[source] | October 1952[source] |
|---|
| First flight | 15 May 1984[source] | 14 January 1950[source] |
|---|
| Retired | 2024 (Italy)[source] | — |
|---|
| Fuel capacity | 3,555 L (939 US gal; 782 imp gal) / 2,700 kg (5,952 lb) internal[source] | — |
|---|
| Wing loading | 512 kg/m 2 (105 lb/sq ft)[source] | 268.5 kg/m 2 (55.0 lb/sq ft)[source] |
|---|
| Thrust/weight | 0.47[source] | 0.63[source] |
|---|
| Rockets | rocket pods[source] | 2 × UB-16 -57 rocket pods for S-5 rockets[source] |
|---|
| Missiles | 2× AIM-9 Sidewinders or MAA-1 Piranha or A-Darter , carried on wingtip rails[source] | — |
|---|
| Bombs | 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | 2 × 250 kg (550 lb) bombs[source] |
|---|
| Guns | 1× 20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon (Italian aircraft) 2× 30 mm (1.181 in) Bernardini Mk-164 cannon (Brazilian aircraft)[source] | 2 × 23 mm (0.906 in) Nudelman-Rikhter NR-23 autocannon (80 rounds per gun, 160 rounds total) 1 × 37 mm Nudelman N-37 autocannon (40 rounds total)[source] |
|---|
| Hardpoints | Bombs: 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | 2 pylons with a capacity of up to 500 kg (1,100 lb) of stores, with provisions to carry combinations of: Rockets: 2 × UB-16 -57 rocket pods for S-5 rockets Bombs: 2 × 250 kg (550 lb) bombs[source] |
|---|
| Developed from | — | Mikoyan-Gurevich MiG-15[source] |
|---|
| Variants | — | PZL-Mielec Lim-6 Shenyang J-5[source] |
|---|
| Developed into | — | Mikoyan-Gurevich MiG-19[source] |
|---|
| Airfoil | — | root: TsAGI S-12; tip: TsAGI SR-11[source] |
|---|
| g limits | — | +8[source] |
|---|
Maximum take-off; MiG-17F · Max takeoff weight
Single source