Statements (60)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbojet engine
|
| gptkbp:aircraft |
multi-role fighter
|
| gptkbp:airlines |
80 kg/s
|
| gptkbp:application |
military aircraft
|
| gptkbp:communityPartnerships |
partnerships with manufacturers
|
| gptkbp:controls |
FADEC
digital electronic control system |
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:designedBy |
Klimov
|
| gptkbp:developer |
derived from RD-33
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:drivetrain |
training programs available
|
| gptkbp:emissionsStandard |
low emissions
|
| gptkbp:energyEfficiency |
high efficiency
|
| gptkbp:engine |
1,200 kg
various aircraft types advanced features quiet operation innovative technology air start pylon-mounted upgrade options available comprehensive support services global sales |
| gptkbp:engineConfiguration |
mass production
single-spool |
| gptkbp:engineDisplacement |
modern design
ongoing development detailed documentation provided |
| gptkbp:engineType |
high performance
high reliability turbofan engine axial compressor certified for military use multiple variants available |
| gptkbp:firstFlight |
2003
|
| gptkbp:fuelCapacity |
2,000 kg/h
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustor |
| gptkbp:hasArea |
extensive testing
|
| gptkbp:hasContent |
300 s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov RD-93
|
| gptkbp:length |
3,000 mm
|
| gptkbp:maintenance |
1,000 hours
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:maxSpeed |
gptkb:Mach_2.0
|
| gptkbp:noise_level |
low noise
|
| gptkbp:operationalRange |
1,500 km
|
| gptkbp:operationalStatus |
1,500 °C
|
| gptkbp:performances |
3,000 hours
|
| gptkbp:propulsion |
no
7.0 84 kN |
| gptkbp:services |
15,000 m
|
| gptkbp:successor |
gptkb:Klimov_RD-33
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedIn |
gptkb:Chengdu_J-10
gptkb:Chengdu_FC-1_Xiaolong |
| gptkbp:weight |
1,200 kg
|