Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
high-altitude reconnaissance aircraft
|
| gptkbp:bore |
105 mm
|
| gptkbp:compressionRatio |
17:1
|
| gptkbp:configuration |
inline six-cylinder
|
| gptkbp:coolingSystem |
gptkb:water
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:developedBy |
Jumo 205
|
| gptkbp:displacement |
16.62 L
|
| gptkbp:engineType |
opposed-piston diesel engine
|
| gptkbp:firstFlight |
1937
|
| gptkbp:fuelType |
diesel
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 207 diesel engines
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notableFeature |
turbocharged
liquid-cooled two-stroke cycle |
| gptkbp:notableFor |
high-altitude performance
|
| gptkbp:powerOutput |
approximately 1,000 hp
|
| gptkbp:stroke |
160 mm
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedIn |
gptkb:Blohm_&_Voss_BV_138
gptkb:Junkers_Ju_86 gptkb:Focke-Wulf_Fw_200 |
| gptkbp:bfsParent |
gptkb:Ju_86R
|
| gptkbp:bfsLayer |
7
|