Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
single-stage fan, 9-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:firstFlight |
1970
|
| gptkbp:length |
4.96 m
|
| gptkbp:manufacturer |
gptkb:Snecma
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
64 kN
95 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Dassault_Mirage_2000
|
| gptkbp:weight |
1,530 kg
|
| gptkbp:bfsParent |
gptkb:Mirage_2000
|
| gptkbp:bfsLayer |
5
|
| http://www.w3.org/2000/01/rdf-schema#label |
Snecma M53-P2 turbofan
|