Rolls-Royce EJ200 jet engine
GPTKB entity
Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.4:1
|
| gptkbp:category |
afterburning turbofan
|
| gptkbp:countryOfOrigin |
gptkb:Germany
gptkb:Italy gptkb:Spain gptkb:United_Kingdom |
| gptkbp:developedBy |
gptkb:Rolls-Royce_Holdings
gptkb:Avio_Aero gptkb:MTU_Aero_Engines gptkb:Industria_de_Turbo_Propulsores |
| gptkbp:diameter |
0.737 m
|
| gptkbp:firstRun |
1991
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce EJ200 jet engine
|
| gptkbp:length |
4 m
|
| gptkbp:manufacturer |
gptkb:EuroJet_Turbo_GmbH
|
| gptkbp:numberOfStages |
1 high-pressure, 1 low-pressure
3 low-pressure, 5 high-pressure |
| gptkbp:relatedTo |
gptkb:Rolls-Royce_RB199
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
60 kN
90 kN |
| gptkbp:usedInAircraft |
gptkb:Eurofighter_Typhoon
|
| gptkbp:weight |
989 kg
|
| gptkbp:bfsParent |
gptkb:Bloodhound_LSR
|
| gptkbp:bfsLayer |
7
|