|
gptkbp:instanceOf
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:Gryazev-Shipunov_GSh-23_cannon
bombs
air-to-air missiles
air-to-surface missiles
|
|
gptkbp:avionics
|
multi-mode radar
|
|
gptkbp:category
|
supersonic aircraft
fourth-generation jet fighter
delta-wing aircraft
single-engine jet
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:combat_range
|
500 km
|
|
gptkbp:countryOfOperation
|
gptkb:India
|
|
gptkbp:designedBy
|
gptkb:Aeronautical_Development_Agency
|
|
gptkbp:ejection_seat
|
gptkb:Martin-Baker_Mk.16L
|
|
gptkbp:emptyWeight
|
6,560 kg
|
|
gptkbp:engine
|
gptkb:General_Electric_F404-GE-IN20
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:export_potential
|
gptkb:Argentina_(interest)
gptkb:Malaysia_(bid)
gptkb:Philippines_(interest)
|
|
gptkbp:firstFlight
|
4 January 2001
|
|
gptkbp:flyByWire
|
yes
|
|
gptkbp:fuelType
|
in-flight refueling capable
|
|
gptkbp:height
|
4.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tejas aircraft
|
|
gptkbp:introduced
|
17 January 2015
|
|
gptkbp:length
|
13.2 m
|
|
gptkbp:manufacturer
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:maximumSpeed
|
Mach 1.8
|
|
gptkbp:maxTakeoffWeight
|
13,500 kg
|
|
gptkbp:nickname
|
gptkb:Tejas
|
|
gptkbp:numberBuilt
|
over 40 (as of 2023)
|
|
gptkbp:origin
|
gptkb:India
|
|
gptkbp:primaryUser
|
gptkb:Indian_Air_Force
gptkb:Indian_Navy
|
|
gptkbp:program_start
|
1983
|
|
gptkbp:radar
|
gptkb:EL/M-2032
gptkb:Uttam_AESA_radar_(planned)
|
|
gptkbp:range
|
1,850 km
|
|
gptkbp:replacedBy
|
gptkb:Mikoyan-Gurevich_MiG-21
|
|
gptkbp:role
|
multirole light fighter
|
|
gptkbp:serviceCeiling
|
15,200 m
|
|
gptkbp:variant
|
gptkb:Tejas_Mk1
gptkb:Tejas_Mk1A
gptkb:Tejas_Mk2
gptkb:Naval_Tejas
|
|
gptkbp:wingspan
|
8.2 m
|
|
gptkbp:bfsParent
|
gptkb:Defence_Research_and_Development_Organisation
|
|
gptkbp:bfsLayer
|
5
|