|
gptkbp:instanceOf
|
trainer aircraft
|
|
gptkbp:aircraft
|
3,000 kg
advanced aerodynamics
high performance
military aircraft
low-wing monoplane
fly-by-wire system
straight wing
jet trainer
training and evaluation
|
|
gptkbp:armament
|
none
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:built
|
over 100
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:constructionMaterial
|
metallic airframe
|
|
gptkbp:crew
|
2
basic to advanced levels
|
|
gptkbp:crew_size
|
gptkb:Martin-Baker_ejection_seat
|
|
gptkbp:design
|
HJT-36
|
|
gptkbp:design_feature
|
high maneuverability
|
|
gptkbp:developer
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:engine
|
gptkb:Kaveri_engine
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:financial_aid
|
ailerons and rudder
|
|
gptkbp:firstFlight
|
2003
|
|
gptkbp:fuel_capacity
|
1,200 liters
|
|
gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
HAL HJT-36 Sitara
|
|
gptkbp:inspiration
|
cost-effective training solution
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Hindustan_Aeronautics_Limited
|
|
gptkbp:maximum_speed
|
650 km/h
|
|
gptkbp:maxTakeoffWeight
|
4,500 kg
|
|
gptkbp:missions
|
training future pilots
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:primaryUser
|
gptkb:Indian_Air_Force
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:role
|
pilot training
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:speed
|
110 km/h
|
|
gptkbp:status
|
in service
|
|
gptkbp:succeededBy
|
30 degrees per second
|
|
gptkbp:surface
|
full-flying tailplane
|
|
gptkbp:takeoffDistance
|
1,200 m
1,000 m
|
|
gptkbp:team
|
advanced jet trainer
HAL design team
|
|
gptkbp:ticketingSystem
|
2007
|
|
gptkbp:training
|
basic flight training
multi-role training
HJT program
|
|
gptkbp:trainTypes
|
HJT-36
|
|
gptkbp:type
|
subsonic
|
|
gptkbp:wingspan
|
10.8 m
|