Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:diameter |
0.65 m
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
2.6 m
|
| gptkbp:manufacturer |
gptkb:Ishikawajima-Harima_Heavy_Industries
|
| gptkbp:numberOfStages |
1
7 |
| gptkbp:status |
out of production
|
| gptkbp:thrust |
15.7 kN
|
| gptkbp:type |
turbojet
|
| gptkbp:usedInAircraft |
gptkb:Fuji_T-1
|
| gptkbp:weight |
430 kg
|
| gptkbp:bfsParent |
gptkb:IHI_Corporation
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
IHI J35 engine
|