Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
annular
|
| gptkbp:configuration |
single-shaft axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
4.7 m
|
| gptkbp:manufacturer |
SNECMA
|
| gptkbp:numberOfStages |
9
|
| gptkbp:status |
out of production
|
| gptkbp:thrust |
10,000 kgf
7,200 kgf dry |
| gptkbp:usedInAircraft |
gptkb:Dassault_Mirage_III
gptkb:Dassault_Mirage_F1 gptkb:Dassault_Mirage_5 |
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:Dassault_Mirage_F1
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
SNECMA Atar 9K-50
|