Nakajima Ha-45 Homare radial engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alternativeName |
Army Type 4
Ha-45 Homare |
| gptkbp:configuration |
two-row radial
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:displacement |
2,362 cubic inches
|
| gptkbp:engineType |
air-cooled radial engine
|
| gptkbp:era |
gptkb:World_War_II
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Nakajima Ha-45 Homare radial engine
|
| gptkbp:manufacturer |
gptkb:Nakajima_Aircraft_Company
|
| gptkbp:notableFor |
high power-to-weight ratio
|
| gptkbp:numberOfEngines |
18
|
| gptkbp:powerOutput |
1,990 hp
|
| gptkbp:usedInAircraft |
gptkb:Kawanishi_N1K-J_Shiden
gptkb:Nakajima_G8N_Renzan gptkb:Nakajima_Ki-84_Hayate gptkb:Nakajima_Ki-87 Nakajima Ki-94-II |
| gptkbp:bfsParent |
gptkb:Nakajima_Ki-84
|
| gptkbp:bfsLayer |
7
|