Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
105 mm
|
| gptkbp:configuration |
rotary
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:displacement |
10.3 L
|
| gptkbp:firstFlight |
1912
|
| gptkbp:fuelType |
gptkb:carburetor
gptkb:gasoline |
| gptkbp:ignition |
magneto
|
| gptkbp:manufacturer |
gptkb:Gnome_et_Rhône
|
| gptkbp:notableFor |
widespread use in World War I aircraft
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
80 hp
|
| gptkbp:productionStartYear |
1912-1918
|
| gptkbp:rpm |
1200
|
| gptkbp:stroke |
140 mm
|
| gptkbp:successor |
Le Rhône 9J rotary engine
|
| gptkbp:usedInAircraft |
gptkb:Nieuport_11
gptkb:Airco_DH.2 gptkb:Sopwith_Pup gptkb:Morane-Saulnier_Type_N gptkb:Fokker_E.III |
| gptkbp:valveConfiguration |
single push-pull rod per cylinder
|
| gptkbp:weight |
122 kg
|
| gptkbp:bfsParent |
gptkb:Morane-Saulnier_Type_H
gptkb:Nieuport_11 gptkb:Morane-Saulnier_Type_N gptkb:Morane-Saulnier_G |
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Le Rhône 9C rotary engine
|