Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Eurofighter_Typhoon
|
| gptkbp:category |
military aircraft engine
|
| gptkbp:countryOfOrigin |
gptkb:Germany
gptkb:Italy gptkb:Spain gptkb:United_Kingdom |
| gptkbp:developedBy |
gptkb:Eurofighter_Typhoon
|
| gptkbp:diameter |
0.737 m
|
| gptkbp:firstFlight |
1991
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
EJ200
|
| gptkbp:length |
4 m
|
| gptkbp:manufacturer |
gptkb:Eurojet_Turbo_GmbH
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
3-stage fan, 5-stage HP compressor
single-stage HP, single-stage LP |
| gptkbp:partner |
gptkb:Rolls-Royce
gptkb:Avio_Aero gptkb:ITP_Aero gptkb:MTU_Aero_Engines |
| gptkbp:status |
in production
|
| gptkbp:thrust |
60 kN
90 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Eurofighter_Typhoon
|
| gptkbp:weight |
989 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:bfsLayer |
5
|