Nakajima Homare 21 radial engine
GPTKB entity
Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
double-row radial
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:displacement |
2,000 cubic inches
|
| gptkbp:engineType |
air-cooled radial engine
|
| gptkbp:firstFlight |
1942
|
| https://www.w3.org/2000/01/rdf-schema#label |
Nakajima Homare 21 radial engine
|
| gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
| gptkbp:numberOfEngines |
18
|
| gptkbp:powerOutput |
2,000 hp
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedInAircraft |
gptkb:Kawanishi_N1K-J_Shiden
gptkb:Nakajima_Ki-84_Hayate gptkb:Yokosuka_P1Y_Ginga |
| gptkbp:bfsParent |
gptkb:Nakajima_C6N
|
| gptkbp:bfsLayer |
6
|