Statements (33)
| 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:displacement |
35 liters
|
| gptkbp:engineType |
liquid-cooled V12 piston engine
|
| gptkbp:firstFlight |
1940
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 213A
|
| gptkbp:length |
2.35 m
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notableFeature |
higher power output than Jumo 211
used in late WWII German aircraft |
| gptkbp:notableVariant |
gptkb:Jumo_213E
gptkb:Jumo_213F gptkb:Jumo_213J Jumo 213C Jumo 213D |
| gptkbp:powerOutput |
1,750 PS
|
| gptkbp:productionStartYear |
1942-1945
|
| gptkbp:stroke |
165 mm
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:Dornier_Do_217
gptkb:Heinkel_He_219 gptkb:Junkers_Ju_188 gptkb:Junkers_Ju_388 gptkb:Focke-Wulf_Fw_190D |
| gptkbp:weight |
900 kg
|
| gptkbp:bfsParent |
gptkb:Jumo_213
gptkb:Junkers_Jumo_213 |
| gptkbp:bfsLayer |
7
|