Rolls-Royce T406-AD-400 turboshaft
GPTKB entity
Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
AE 1107C-Liberty
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.6 m
|
| gptkbp:firstFlight |
1989
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce T406-AD-400 turboshaft
|
| gptkbp:length |
2.1 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:powerOutput |
6,150 shaft horsepower
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_Boeing_V-22_Osprey
|
| gptkbp:weight |
1,194 kg
|
| gptkbp:bfsParent |
gptkb:CV-22B
|
| gptkbp:bfsLayer |
7
|