Nakajima Sakae 21 radial engine
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
130 mm
|
| gptkbp:configuration |
two-row radial
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:displacement |
27.87 L
|
| gptkbp:engineType |
air-cooled radial engine
|
| gptkbp:firstFlight |
1941
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
| gptkbp:numberOfEngines |
14
|
| gptkbp:powerOutput |
1130 hp
|
| gptkbp:predecessor |
gptkb:Nakajima_Sakae_12_radial_engine
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
Nakajima Homare engine
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:Nakajima_Ki-43
gptkb:Nakajima_Ki-84 gptkb:Mitsubishi_A6M_Zero |
| gptkbp:bfsParent |
gptkb:A6M3
gptkb:A6M5 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Nakajima Sakae 21 radial engine
|