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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Indian_Air_Force_aircraft
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gptkbp:aircraft_operated
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gptkb:Group_Captain_S._R._S._S._Rao
gptkb:Wing_Commander_A._K._Rao
gptkb:Wing_Commander_A._K._S._S._S._Rao
gptkb:Wing_Commander_A._S._S._Rao
gptkb:Wing_Commander_R._S._Rao
gptkb:Wing_Commander_R._S._S._Rao
gptkb:Wing_Commander_S._R._Rao
gptkb:Wing_Commander_S._R._S._Rao
gptkb:Wing_Commander_S._S._Rao
gptkb:Wing_Commander_S._S._S._Rao
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|
gptkbp:armament
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Bombs
Air-to-air missiles
Air-to-ground missiles
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gptkbp:avionics
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gptkb:radar_system
gptkb:aircraft
Digital fly-by-wire system
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|
gptkbp:cockpit
|
Glass cockpit
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|
gptkbp:combat_radius
|
500 km
|
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gptkbp:country
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gptkb:India
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gptkbp:crew
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gptkb:musical
|
|
gptkbp:design
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gptkb:2016
Single-engine
Delta wing
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|
gptkbp:developer
|
gptkb:DRDO
gptkb:Indian_Air_Force
|
|
gptkbp:engine
|
gptkb:General_Electric_F404
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|
gptkbp:first_flight
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gptkb:2023
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gptkbp:fuel_capacity
|
3,200 liters
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|
https://www.w3.org/2000/01/rdf-schema#label
|
LCA Tejas Mk II
|
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gptkbp:landing_gear
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Retractable
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gptkbp:length
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13.2 meters
|
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gptkbp:manufacturer
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:max_takeoff_weight
|
14,500 kg
|
|
gptkbp:number_built
|
Expected to be around 83
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:role
|
Reconnaissance
Multirole fighter
Air superiority
Ground attack
|
|
gptkbp:sensor
|
Synthetic aperture radar
Electro-optical targeting system
Infrared search and track
|
|
gptkbp:service_ceiling
|
15,000 meters
|
|
gptkbp:services
|
Expected in 2025
|
|
gptkbp:stealth_features
|
Reduced radar cross-section
|
|
gptkbp:successor
|
gptkb:Mikoyan_Mi_G-21
gptkb:HAL_Ajeet
|
|
gptkbp:variant
|
gptkb:LCA_Tejas_Mk_I
gptkb:LCA_Tejas_Mk_I(A)
|
|
gptkbp:weight
|
6,500 kg
|
|
gptkbp:wingspan
|
14.6 meters
|