Rolls-Royce Gem 42-1 turboshaft
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.48 m
|
| gptkbp:fuelType |
Aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Gem 42-1 turboshaft
|
| gptkbp:introducedIn |
1970s
|
| gptkbp:length |
1.7 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
compact design
|
| gptkbp:numberOfStages |
3 axial, 1 centrifugal
2 high-pressure, 1 power turbine |
| gptkbp:powerOutput |
~1120 shp
|
| gptkbp:usedIn |
gptkb:Westland_Lynx
|
| gptkbp:weight |
170 kg
|
| gptkbp:bfsParent |
gptkb:Sea_Lynx_Mk88A
|
| gptkbp:bfsLayer |
6
|