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]
Tejas Mk-1A · Length
Single sourceConfiguration
| Specification | AMX International AMX | HAL Tejas |
|---|---|---|
| Type | Ground-attack aircraft[source] | Multirole light fighter[source] |
| National origin | Italy / Brazil[source] | India[source] |
| Manufacturer | AMX International[source] | Hindustan Aeronautics Limited[source] |
| Status | Active service[source] | In service |
13.2 m (43 ft 4 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; Tejas Mk-1A · Empty weight
Single sourceGross; Tejas Mk-1A · Gross weight
Single sourceAMX · 1 × Rolls-Royce Spey 807 turbofan engine thrust
Single source1 × Rolls-Royce Spey 807 turbofan engine, 49.1 kN (11,000 lbf) thrust[source]
Tejas Mk-1A · 1 × General Electric F404-GE-IN20 afterburning turbofan with FADEC with afterburner
Single source1 × General Electric F404-GE-IN20 afterburning turbofan with FADEC , 85 kN (19,000 lbf) with afterburner[source]
AMX · Endurance
Single source4 hours, 15 minutes[source]
AMX · 10,260 ft/min
Single source52.1 m/s (10,260 ft/min)[source]
Tejas Mk-1A · external stores
Single source4,500 kg (9,900 lb) – 5,300 kg (11,700 lb) external stores[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] | — |
|---|
| Number built | 230[source] | 45 (plus 17 prototypes)[source] |
|---|
| Manufactured | 1986–1999[source] | 2001–present[source] |
|---|
| Introduction date | 1989[source] | 17 January 2015[source] |
|---|
| First flight | 15 May 1984[source] | 4 January 2001[source] |
|---|
| Retired | 2024 (Italy)[source] | — |
|---|
| Fuel capacity | 3,555 L (939 US gal; 782 imp gal) / 2,700 kg (5,952 lb) internal[source] | 2,458 kg (5,419 lb)3,060 L (670 imp gal; 810 US gal) internal; 2 × 1,200 L (260 imp gal; 320 US gal), 800 L (180 imp gal; 210 US gal) drop tank inboard, 725 L (159 imp gal; 192 US gal) drop tank under fuselage[source] |
|---|
| Wing loading | 512 kg/m 2 (105 lb/sq ft)[source] | 255.2 kg/m 2 (52.3 lb/sq ft)[source] |
|---|
| Thrust/weight | 0.47[source] | 1.07[source] |
|---|
| Rockets | rocket pods[source] | — |
|---|
| Missiles | 2× AIM-9 Sidewinders or MAA-1 Piranha or A-Darter , carried on wingtip rails[source] | Air-to-air missiles : 2 × R-73 4 × I-Derby ER 2 × Python-5 4 × Astra Mk 1 4 × Astra Mk 2 (Planned) 4 × ASRAAM 4 × Meteor (Planned) Air-to-surface missile : AASM-Hammer (SBU-38/54/64) 2 × BrahMos-NG ALCM (Planned) SCALP-EG (Planned) Anti-radiation missile : 2 × Rudram-1 (Planned) Anti-ship missile : 2 × NASM-MR[source] |
|---|
| Bombs | 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | Precision-guided munition : Spice Joint Direct Attack Munition HSLD-100/250/450/500 Gaurav (glide bomb) Smart Anti-Airfield Weapon Tactical Advanced Range Augmentation Al Tariq-LR (potential) Laser-guided bomb : GBU-16 Paveway II Sudarshan Griffin LGB Cluster munition :[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] | 1 × 23 mm twin-barrel GSh-23 cannon with 220 rounds[source] |
|---|
| Hardpoints | Bombs: 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | 9 with a capacity of 5300 kg, with provisions to carry combinations of: Missiles: Air-to-air missiles : 2 × R-73 4 × I-Derby ER 2 × Python-5 4 × Astra Mk 1 4 × Astra Mk 2 (Planned) 4 × ASRAAM 4 × Meteor (Planned) Air-to-surface missile : AASM-Hammer (SBU-38/54/64) 2 × BrahMos-NG ALCM (Planned) SCALP-EG (Planned) Anti-radiation missile : 2 × Rudram-1 (Planned) Anti-ship missile : 2 × NASM-MR Bombs: Precision-guided munition : Spice Joint Direct Attack Munition HSLD-100/250/450/500 Gaurav (glide bomb) Smart Anti-Airfield Weapon Tactical Advanced Range Augmentation Al Tariq-LR (potential) Laser-guided bomb : GBU-16 Paveway II Sudarshan Griffin LGB Cluster munition : BDL Chaff / Flare Counter Measure Dispensing System (CMDS) DARE Targeting pod (Tejas Mk.1 FOC) Rafael Litening III[source] |
|---|
| Designer | — | Aeronautical Development Agency Aircraft Research and Design Centre ( HAL )[source] |
|---|
| Primary user | — | Indian Air Force[source] |
|---|
| Developed into | — | HAL Tejas Mk2 HAL TEDBF[source] |
|---|
| g limits | — | +9/-3.5[source] |
|---|
| Air-to-air missiles | — | 2 × R-73 4 × I-Derby ER 2 × Python-5 4 × Astra Mk 1 4 × Astra Mk 2 (Planned) 4 × ASRAAM 4 × Meteor (Planned)[source] |
|---|
| Air-to-surface missile | — | AASM-Hammer (SBU-38/54/64) 2 × BrahMos-NG ALCM (Planned) SCALP-EG (Planned)[source] |
|---|
| Anti-radiation missile | — | 2 × Rudram-1 (Planned)[source] |
|---|
| Anti-ship missile | — | 2 × NASM-MR[source] |
|---|
| Precision-guided munition | — | Spice Joint Direct Attack Munition HSLD-100/250/450/500 Gaurav (glide bomb) Smart Anti-Airfield Weapon Tactical Advanced Range Augmentation Al Tariq-LR (potential)[source] |
|---|
| Laser-guided bomb | — | GBU-16 Paveway II Sudarshan Griffin LGB[source] |
|---|
Maximum take-off; Tejas Mk-1A · Max takeoff weight
Single source