Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
150 mm
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:configuration |
inverted V12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:developedBy |
gptkb:Jumo_213A
|
| gptkbp:displacement |
35 liters
|
| gptkbp:engineType |
liquid-cooled V12
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 213E
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:powerOutput |
1,750 PS
|
| gptkbp:stroke |
165 mm
|
| gptkbp:supercharger |
two-stage, three-speed
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedIn |
gptkb:Focke-Wulf_Ta_152
gptkb:Dornier_Do_335 |
| gptkbp:weight |
970 kg
|
| gptkbp:bfsParent |
gptkb:Jumo_213
gptkb:Junkers_Jumo_213 |
| gptkbp:bfsLayer |
7
|