Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustorType |
annular
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.69 m
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
M88 engine
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Safran_Aircraft_Engines
|
| gptkbp:notableFeature |
modular design
full authority digital engine control (FADEC) low infrared signature |
| gptkbp:numberOfStages |
3 low-pressure, 6 high-pressure
single high-pressure, single low-pressure |
| gptkbp:status |
in service
|
| gptkbp:thrust |
50 kN
75 kN |
| gptkbp:type |
turbofan
|
| gptkbp:usedIn |
gptkb:Dassault_Rafale
|
| gptkbp:weight |
897 kg
|
| gptkbp:bfsParent |
gptkb:Snecma
gptkb:Safran |
| gptkbp:bfsLayer |
6
|