Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_250-C30
|
| gptkbp:application |
helicopters
|
| gptkbp:controls |
electronic control system
|
| gptkbp:cooling_system |
air-cooled
direct air cooling |
| gptkbp:diameter |
0.4 m
|
| gptkbp:engine_type |
axial compressor
single-stage turbine |
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 250-C47
|
| gptkbp:length |
1.2 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_users |
gptkb:Agusta_Westland
gptkb:Sikorsky_Aircraft gptkb:Bell_Helicopter gptkb:Eurocopter gptkb:Mc_Donnell_Douglas |
| gptkbp:power_output |
450 shp
|
| gptkbp:powers |
3.0 k W/kg
|
| gptkbp:setting |
gptkb:engine
|
| gptkbp:weight |
150 kg
|