Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
150 mm
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:configuration |
V12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:developedBy |
gptkb:World_War_II
|
| gptkbp:displacement |
35 liters
|
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
aviation gasoline
direct fuel injection |
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notableVariant |
gptkb:Jumo_213A
gptkb:Jumo_213E gptkb:Jumo_213F |
| gptkbp:powerOutput |
1750 hp
|
| gptkbp:predecessor |
gptkb:Jumo_211
|
| gptkbp:stroke |
165 mm
|
| gptkbp:successor |
gptkb:Jumo_222
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:type |
liquid-cooled engine
|
| gptkbp:usedIn |
gptkb:Heinkel_He_219
gptkb:Junkers_Ju_188 gptkb:Focke-Wulf_Fw_190_D gptkb:Junkers_Ju_388 gptkb:Dornier_Do_335 |
| gptkbp:valvetrain |
four valves per cylinder
|
| gptkbp:weight |
900 kg
|
| gptkbp:bfsParent |
gptkb:Junkers_Ju_188
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 213
|