Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:firstFlight |
1957
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
SNECMA Atar 9C turbojet
|
| gptkbp:length |
4.7 m
|
| gptkbp:manufacturer |
SNECMA
|
| gptkbp:numberOfStages |
9
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
yes
6,000 kgf (13,230 lbf) |
| gptkbp:usedInAircraft |
gptkb:Dassault_Mirage_III
gptkb:Dassault_Mirage_5 gptkb:Dassault_Mirage_50 |
| gptkbp:weight |
1,350 kg
|
| gptkbp:bfsParent |
gptkb:Mirage_V
gptkb:Dassault_Mirage_5 gptkb:Mirage_IIID gptkb:Mirage_IIIO |
| gptkbp:bfsLayer |
7
|