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Engine - US
Avionics - (French/Isreal/Indian)
Weapons - Israel
The LCA integrates modern design concepts like static instability, digital fly-by-wire flight control system, integrated avionics, glass cockpit, primary composite structure, multi-mode radar, microprocessor based utility and brake management systems.
Wing Span 8.20 m
Length 13.20 m
Empty Weight 5500 kg
Engine - GE F404-F2J3 turbofan r
Fuel Capacity Internal fuel capacity - 3000 liters
Centerline and the two-inner hardpoints under each wing can carry five 800 liters fuel tanks
also has an in-flight refuelling probe
Maximum Range - 850 Kms
Maximum Speed Mach 1.7
Service Ceiling 50,000 feet.
G Limits +9/-3.5
Armament internally mounted GSh-23mm twin barrel gun with 220 rounds of ammunition
Seven external hardpoints, can carry air-to-air missiles, air-to-surface missiles, anti-ship missiles, rocket launchers and ECM pods
Maximum External Stores Load 4000kg (8818 lbs.)
Self Defence RWR system, jammer and chaff & flare dispensers



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