Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Lockheed_Martin_C-130J_Super_Hercules
|
| gptkbp:category |
Aircraft engines
Turboprop engines |
| gptkbp:compressionRatio |
14-stage axial
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.67 m
|
| gptkbp:family |
gptkb:Rolls-Royce_AE_2100
|
| gptkbp:firstFlight |
1996
|
| gptkbp:fuelType |
Aviation kerosene
|
| gptkbp:length |
2.49 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:powerOutput |
4,637 shp
|
| gptkbp:propulsion |
Dowty R391 six-bladed composite
|
| gptkbp:relatedTo |
gptkb:Rolls-Royce_AE_2100D3
Rolls-Royce AE 2100P |
| gptkbp:usedIn |
gptkb:Alenia_C-27J_Spartan
gptkb:Lockheed_Martin_C-130J_Super_Hercules |
| gptkbp:weight |
740 kg
|
| gptkbp:bfsParent |
gptkb:ShinMaywa_US-2
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 2100J
|