Properties (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbo-shaft engine
|
| gptkbp:application |
helicopters
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
0.3 m
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:engineConfiguration |
single-spool
|
| gptkbp:engineType |
4
free turbine turbo-shaft C20A C20B C20C C20D C20F C20G C20H C20I C20J C20K C20M C20O C20P C20Q C20R C20S C20T C20V C20Y C20Z C20W C20E C20L C20N C20U C20X |
| gptkbp:firstFlight |
1960
|
| gptkbp:fuel_capacity |
0.5 kg/shp/hr
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 250-C20
|
| gptkbp:launchSite |
electric starter
|
| gptkbp:length |
1.1 m
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:maximum_speed |
42000
|
| gptkbp:notableUsers |
gptkb:McDonnell_Douglas
gptkb:Bell_Helicopter gptkb:Sikorsky AgustaWestland Eurocopter |
| gptkbp:operationalRange |
2000 hours
|
| gptkbp:powerOutput |
420 shp
|
| gptkbp:powers |
0.95 shp/kg
|
| gptkbp:related_engine |
gptkb:Rolls-Royce_250
|
| gptkbp:weight |
120 kg
|