|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
low-wing
trainer
jet trainer
|
|
gptkbp:armament
|
none
|
|
gptkbp:climbRate
|
10 m/s
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:crew_size
|
2
|
|
gptkbp:decommissioned
|
still in service
|
|
gptkbp:design
|
gptkb:India
HAL
basic trainer
|
|
gptkbp:engine
|
gptkb:Adour_Mk_811
2
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:firstFlight
|
1989
|
|
gptkbp:firstGeneration
|
1990
|
|
gptkbp:fuelCapacity
|
1,500 liters
|
|
gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kiran Mk II
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:maxSpeed
|
650 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,500 kg
|
|
gptkbp:numberBuilt
|
around 200
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:primaryUser
|
gptkb:Indian_Air_Force
|
|
gptkbp:productionStartYear
|
1989
|
|
gptkbp:productionYears
|
2005
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
1990
10,000 m
|
|
gptkbp:speed
|
110 km/h
|
|
gptkbp:status
|
in service
|
|
gptkbp:succeededBy
|
30°/s
|
|
gptkbp:successor
|
gptkb:HAL_HJT-36_Sitara
|
|
gptkbp:supportRole
|
pilot training
|
|
gptkbp:takeoffDistance
|
1,200 m
1,000 m
|
|
gptkbp:usedBy
|
gptkb:Indian_Air_Force
|
|
gptkbp:variant
|
gptkb:Kiran_Mk_I
|
|
gptkbp:wingArea
|
30 m²
|
|
gptkbp:wingspan
|
10.5 m
|