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HAL Tejas ✕ Dassault Mirage III ✕
Manufacturer Hindustan Aeronautics Limited Commonwealth Aircraft Corporation
Description The HAL Tejas () is an Indian single-engine, 4.5 generation, delta wing, multirole combat aircraft designed by the Aeronautical Development Agency and manufactured by Hindustan Aeronautics Limited (HAL) for the Indian Air Force (IAF) and the Indian Navy. The Dassault Mirage III () is a family of single/dual-seat, single-engine, fighter aircraft developed and manufactured by French aircraft company Dassault Aviation.
First Flight 2001-01-04 1956-11-17
Entry Into service 2015-01-17 1961-01-01
Designer Hindustan Aeronautics Limited Commonwealth Aircraft Corporation
Type Multirole light fighter
Length (m) 13.2 15.03
Height (m) 4.4 4.5
Cockpit Crew 1 1
Max Speed (km/h) 2220 2350
Max Ceiling (m) 16000 17000
Rate of Climb (m/s) 83
Armament 1 × 23 mm twin-barrel GSh-23 cannon with 220 rounds; 9 2 × 30 mm DEFA 552 cannon with 125 rounds per gun; 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.; 2 × Matra JL-100 drop tank/rocket pack, each with 19× 68 mm SNEB rockets and 250 L of fuel; 2 × AIM-9B Sidewinder Air to Air missiles (AAM) or; 2 × …
Max Mach (Mach) 1.8 2.2
National Origin India France
Number Built 45 1422
Powerplant Description 1 × General Electric F404-GE-IN20 afterburning turbofan with FADEC 1 × SNECMA Atar 09C afterburning turbojet engine, 41.97 kN thrust each
Primary Users Indian Air Force French Air Force (historical), Royal Australian Air Force (historical), Pakistan Air Force , Israeli Air Force (historical)
Status In service In service with the Pakistan Air Force
Wikipedia Article (URL) en.wikipedia.org/wiki/HAL_Tejas en.wikipedia.org/wiki/Dassault_Mirage_III
Flat Wing Span (m) 8.2 8.22
Flat Wing Area (m²) 38.4 34.85
Aircraft Engine General Electric F404
Number of Engines 1 1