Rolls-Royce AE 1107C-Liberty turboshaft
GPTKB entity
Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
gptkb:military
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:family |
Rolls-Royce AE 1107
|
| gptkbp:firstFlight |
1990s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 1107C-Liberty turboshaft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:powerOutput |
6,150 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_Boeing_V-22_Osprey
gptkb:Bell_V-280_Valor |
| gptkbp:bfsParent |
gptkb:Bell_V-22_Osprey
gptkb:Bell_Boeing_MV-22B_Osprey |
| gptkbp:bfsLayer |
7
|