Statements (28)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:challenge |
reliability issues
weight issues afterburner performance |
gptkbp:collaboratedWith |
gptkb:Snecma
|
gptkbp:countryOfOrigin |
gptkb:India
|
gptkbp:developedBy |
gptkb:Gas_Turbine_Research_Establishment
|
gptkbp:diameter |
0.9 m
|
gptkbp:firstRun |
1996
|
gptkbp:fuelType |
aviation kerosene
|
https://www.w3.org/2000/01/rdf-schema#label |
Kaveri Engine
|
gptkbp:intendedUse |
gptkb:HAL_Tejas
|
gptkbp:length |
3.8 m
|
gptkbp:notableFor |
indigenous Indian jet engine program
|
gptkbp:numberOfAxles |
2
|
gptkbp:numberOfFanStages |
1
|
gptkbp:numberOfStages |
1
6 |
gptkbp:relatedTo |
GTX-35VS Kaveri
Kaveri Marine Gas Turbine |
gptkbp:status |
under development
|
gptkbp:thrust |
52 kN
81 kN |
gptkbp:type |
afterburning turbofan
|
gptkbp:usedIn |
Ghatak UCAV (planned)
|
gptkbp:weight |
1236 kg
|
gptkbp:bfsParent |
gptkb:Gas_Turbine_Research_Establishment_(GTRE)
|
gptkbp:bfsLayer |
6
|