Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:application |
gptkb:Aérospatiale_SA_315_Lama
gptkb:SA_330_Puma |
| gptkbp:compression_ratio |
8:1
|
| gptkbp:configuration |
free turbine
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
0.4 m
|
| gptkbp:engine_type |
turboshaft
|
| gptkbp:first_flight |
gptkb:1955
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Astazou 50
|
| gptkbp:length |
1.2 m
|
| gptkbp:manufacturer |
gptkb:Aérospatiale
|
| gptkbp:number_of_stages |
2
|
| gptkbp:operational_history |
used in military and civilian aviation.
|
| gptkbp:power_output |
500 hp
|
| gptkbp:role |
gptkb:turbofan_engine
|
| gptkbp:torque |
1000 Nm
|
| gptkbp:used_in |
helicopters
|
| gptkbp:weight |
150 kg
|
| gptkbp:bfsParent |
gptkb:Turbomeca_Astazou
|
| gptkbp:bfsLayer |
7
|