Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.91 m
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Snecma M53-P2
|
| gptkbp:length |
4.96 m
|
| gptkbp:manufacturer |
gptkb:Snecma
|
| gptkbp:notableFeature |
designed for supersonic flight
|
| gptkbp:numberOfAxles |
single-shaft
|
| gptkbp:numberOfStages |
9-stage axial compressor
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Snecma_M88
|
| gptkbp:thrust |
64 kN dry
98 kN with afterburner |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Dassault_Mirage_2000
|
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:Mirage_2000-9
|
| gptkbp:bfsLayer |
6
|