|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:challenges
|
faced several technical challenges
|
|
gptkbp:civilian_application
|
potential for civilian aircraft
|
|
gptkbp:collaboration
|
gptkb:ISRO
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:component_testing
|
completed
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
digital electronic control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:design
|
completed
|
|
gptkbp:designed_by
|
gptkb:DRDO
|
|
gptkbp:development
|
gptkb:1996
ongoing
|
|
gptkbp:elevation
|
up to 15,000 m
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
Brayton cycle
|
|
gptkbp:engine_power
|
approximately 4,000 hours
|
|
gptkbp:fuel_type
|
Aviation Turbine Fuel (ATF)
|
|
gptkbp:funding
|
government funded
|
|
gptkbp:future_plans
|
upgraded variants
|
|
gptkbp:goal
|
indigenous development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kaveri engine
|
|
gptkbp:integration
|
integrated into Tejas aircraft
|
|
gptkbp:invention
|
multiple patents filed
Kaveri K9
|
|
gptkbp:is_tested_for
|
DRDO facilities
ongoing performance testing
|
|
gptkbp:maintenance
|
requires regular maintenance
|
|
gptkbp:manufacturer
|
gptkb:HAL
|
|
gptkbp:max_speed
|
Mach 1.1
|
|
gptkbp:military_technology
|
gptkb:military_aircraft
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:original_run
|
gptkb:2010
|
|
gptkbp:part_of
|
Indian Air Force's Tejas program
|
|
gptkbp:participating_nations
|
growing interest from other countries
|
|
gptkbp:performance_goal
|
to achieve 90 k N thrust
|
|
gptkbp:project
|
Kaveri project
|
|
gptkbp:propulsion
|
around 80 k N
|
|
gptkbp:related_aircraft
|
light combat aircraft
|
|
gptkbp:research_focus
|
aero-thermodynamics
|
|
gptkbp:research_institutes
|
various Indian research institutes
|
|
gptkbp:successor
|
Kaveri Mk2
|
|
gptkbp:sustainability
|
focus on sustainable aviation
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:upgrades
|
planned future upgrades
|
|
gptkbp:used_in
|
gptkb:Tejas_aircraft
|
|
gptkbp:weight
|
approximately 1,000 kg
|
|
gptkbp:bfsParent
|
gptkb:HAL-Tejas
gptkb:Tejas_Trainer
|
|
gptkbp:bfsLayer
|
6
|