Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:C-27_J_Spartan
gptkb:Lockheed_Martin_C-130_J_Super_Hercules gptkb:KC-130_Hercules gptkb:C-130_J_Super_Hercules gptkb:C-130_Hercules |
| gptkbp:application |
regional aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1,200 mm
|
| gptkbp:engine_type |
free turbine
axial compressor |
| gptkbp:first_flight |
gptkb:1996
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 2100 D3
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:power_output |
4,600 shp
|
| gptkbp:propulsion |
4,600 lbf
|
| gptkbp:setting |
twin-shaft
|
| gptkbp:used_in |
gptkb:Lockheed_Martin_C-130_J_Super_Hercules
|
| gptkbp:weight |
1,200 lb
|