Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:features |
thrust vectoring nozzle
low bypass ratio high power generator stealth compatible design |
| gptkbp:firstFlight |
2018
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:length |
4.8 m
|
| gptkbp:manufacturer |
gptkb:IHI_Corporation
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:thrust |
15 tons
11 tons |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:F-X_(Japan)
gptkb:Mitsubishi_X-2_Shinshin |
| gptkbp:weight |
2,000 kg
|
| gptkbp:bfsParent |
gptkb:IHI_Corporation
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
IHI XF9 engine
|