Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboprop engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
1,200 mm
|
| gptkbp:engineType |
axial
free turbine |
| gptkbp:firstFlight |
1996
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 2100D3
|
| gptkbp:is_used_in |
gptkb:Lockheed_Martin_C-130J_Super_Hercules
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:powerOutput |
4,600 shp
|
| gptkbp:setting |
twin-shaft
|
| gptkbp:weight |
1,200 lb
|