Oberursel Ur.II rotary engine
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:basedOn |
gptkb:Gnome_Monosoupape_9N
|
| gptkbp:configuration |
rotary
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:German_Empire
|
| gptkbp:displacement |
16.3 L
|
| gptkbp:era |
gptkb:World_War_I
|
| gptkbp:firstFlight |
1914
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Oberursel Ur.II rotary engine
|
| gptkbp:manufacturer |
gptkb:Oberursel
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
110 hp
|
| gptkbp:usedInAircraft |
gptkb:Fokker_Dr.I
gptkb:Fokker_D.VI Siemens-Schuckert D.III |
| gptkbp:weight |
145 kg
|
| gptkbp:bfsParent |
gptkb:Fokker_D.VIII
|
| gptkbp:bfsLayer |
7
|