Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
150 mm
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:displacement |
35 liters
|
| gptkbp:engineType |
liquid-cooled
V-12 |
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notableFeature |
high-altitude performance
|
| gptkbp:powerOutput |
1750 hp
|
| gptkbp:predecessor |
gptkb:Jumo_211
|
| gptkbp:productionStartYear |
1942-1945
|
| gptkbp:stroke |
165 mm
|
| gptkbp:successor |
gptkb:Jumo_222
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:Dornier_Do_217
gptkb:Heinkel_He_219 gptkb:Junkers_Ju_188 gptkb:Focke-Wulf_Fw_190D |
| gptkbp:bfsParent |
gptkb:Junkers_Ju_388
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 213 inline engine
|