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gptkbp:instanceOf
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aircraft
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|
gptkbp:aircraft
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gptkb:Hindustan_Aeronautics_Limited
4.5 m
in production
advanced training
military aircraft
2,500 kg
12.5 m
single-engine
trainer
11.5 m
basic and advanced flight training
HJT-16
|
|
gptkbp:airlines
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2
|
|
gptkbp:armament
|
none
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gptkbp:avionics
|
modernized cockpit instruments
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|
gptkbp:cockpit
|
tandem_seating
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|
gptkbp:crew
|
2
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|
gptkbp:decommissioned
|
still in service
|
|
gptkbp:design
|
low-wing monoplane
HAL engineers
|
|
gptkbp:developer
|
Indian_Air_Force_requirements
|
|
gptkbp:engine
|
1
HAL HTFE-25
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:firstFlight
|
1989
|
|
gptkbp:firstGeneration
|
1990
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gptkbp:fuelCapacity
|
1,200 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
HJT-16 Kiran
|
|
gptkbp:landingGear
|
tricycle type
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:maximumDepth
|
1,000 kg
10 m/s
|
|
gptkbp:maxRange
|
1,500 km
|
|
gptkbp:maxSpeed
|
550 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
|
|
gptkbp:numberBuilt
|
around 100
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:primaryUser
|
gptkb:Indian_Air_Force
|
|
gptkbp:productionStartYear
|
1989
|
|
gptkbp:releaseYear
|
1988
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
1990
10,000 m
|
|
gptkbp:speed
|
100 km/h
|
|
gptkbp:succeededBy
|
30°/s
|
|
gptkbp:successor
|
HAL Tejas
|
|
gptkbp:supportRole
|
basic flight training
|
|
gptkbp:training
|
2 pilots
|
|
gptkbp:variant
|
gptkb:HJT-16_Kiran_Mk_II
|
|
gptkbp:wingArea
|
30 m²
|
|
gptkbp:wingspan
|
11.5 m
|