Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
helicopters
|
| gptkbp:compression_ratio |
12:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:engine_configuration |
free turbine
|
| gptkbp:first_flight |
gptkb:1970
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca TM 319 engine
|
| gptkbp:length |
1.2 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:number_of_stages |
2
|
| gptkbp:propulsion |
700 lbf
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Aérospatiale_SA_315_Lama
|
| gptkbp:weight |
150 kg
|
| gptkbp:bfsParent |
gptkb:Turbomeca
|
| gptkbp:bfsLayer |
6
|