Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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
|
https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 2100J
|
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
|