Properties (53)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aimsTo |
reduce dependency on foreign engines
|
| gptkbp:aircraft |
multirole combat aircraft
|
| gptkbp:collaborations |
various_Indian_research_institutions
|
| gptkbp:component |
Indian_defense_PSUs
|
| gptkbp:controls |
digital electronic control system
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:country |
gptkb:India
|
| gptkbp:design |
completed
|
| gptkbp:designedBy |
gptkb:DRDO
|
| gptkbp:developer |
ongoing
over 20 years technical hurdles |
| gptkbp:energyEfficiency |
improving over iterations
|
| gptkbp:engineConfiguration |
single_spool
|
| gptkbp:engineType |
axial compressor
high-pressure turbine |
| gptkbp:environmentalImpact |
lower emissions
|
| gptkbp:firstFlight |
conducted in 2014
|
| gptkbp:firstRace |
2010
|
| gptkbp:fuelType |
annular combustor
Aviation Turbine Fuel (ATF) |
| gptkbp:futurePlans |
upgraded variants
advanced fighter aircraft engine higher thrust variants |
| gptkbp:goal |
indigenous fighter aircraft engine
|
| gptkbp:hasArea |
promising performance
DRDO_facilities |
| https://www.w3.org/2000/01/rdf-schema#label |
Kaveri engine
|
| gptkbp:inspiration |
global jet engine technology
|
| gptkbp:integration |
with_HAL_Tejas_aircraft
|
| gptkbp:keyFigures |
self-reliance in defense technology
|
| gptkbp:keyPeople |
aerospace engineers
|
| gptkbp:manufacturer |
gptkb:Hindustan_Aeronautics_Limited
|
| gptkbp:notableContestants |
hot test in 2016
|
| gptkbp:notableFeature |
indigenous technology
|
| gptkbp:partnerships |
international_aerospace_companies
|
| gptkbp:partOf |
Kaveri program
|
| gptkbp:performance |
high thrust-to-weight ratio
|
| gptkbp:productionCompany |
1996
|
| gptkbp:productionStartYear |
around 100 kN
|
| gptkbp:project |
2025
|
| gptkbp:propulsion |
around 80 kN
|
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:relatedAircraft |
gptkb:Kiran_Mk_II
|
| gptkbp:research |
gptkb:government_of_India
|
| gptkbp:researchFocus |
aerodynamics and materials
|
| gptkbp:status |
in development
|
| gptkbp:strategicGoals |
national security
|
| gptkbp:technology |
classified
|
| gptkbp:type |
turbofan engine
|
| gptkbp:usedIn |
HAL Tejas
|
| gptkbp:weight |
approximately 1,200 kg
|