Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:transport_aircraft
|
| gptkbp:armament |
gptkb:6
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:configuration |
four-shaft engine
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:development |
European consortium
|
| gptkbp:diameter |
1,200 mm
|
| gptkbp:emissions_standard |
low
|
| gptkbp:first_flight |
gptkb:2005
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
TP400-D6
|
| gptkbp:length |
2,800 mm
|
| gptkbp:maintenance |
3,000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
low
|
| gptkbp:power_output |
8,000 shp
|
| gptkbp:propulsion |
11,000 lbf
|
| gptkbp:reliability |
high
|
| gptkbp:service_entry |
gptkb:2009
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Airbus_A400_M
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:A-400_M
gptkb:A400_M gptkb:A400_M_Atlas |
| gptkbp:bfsLayer |
5
|