Nakajima Homare

GPTKB entity

Statements (50)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:aircraft gptkb:Mitsubishi_G4M
Kawasaki Ki-61
Yokosuka D4Y
gptkbp:application military aviation
gptkbp:compressionRatio 6.5:1
gptkbp:coolingSystem air-cooled
air-cooled design
gptkbp:cylinderCount 14-cylinder
gptkbp:design_feature high reliability
robust construction
large displacement
gptkbp:displacement 1,900 cubic inches
gptkbp:engine fighter aircraft
bomber aircraft
transport aircraft
training aircraft
reconnaissance aircraft
ground attack aircraft
naval aircraft
radial layout
special mission aircraft
night fighter aircraft
torpedo bomber aircraft
gptkbp:engineConfiguration 14-cylinder configuration
gptkbp:engineType two-row radial engine
gptkbp:firstFlight 1939
gptkbp:fuelType spark ignition
aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Nakajima Homare
gptkbp:introduced 1940
gptkbp:is_used_in gptkb:Mitsubishi_A6M_Zero
gptkbp:manufacturer gptkb:Nakajima_Aircraft_Company
gptkbp:notable_feature Homare 21
Homare_12
Homare_30
gptkbp:notableUsers gptkb:Imperial_Japanese_Navy
gptkb:Imperial_Japanese_Army_Air_Service
gptkbp:operationalHistory gptkb:World_War_II
gptkbp:origin gptkb:Japan
gptkbp:performance high power-to-weight ratio
gptkbp:performances high_altitude_performance
gptkbp:powerOutput 1,000 to 2,000 hp
gptkbp:produces over 10,000 units
gptkbp:productionYears 1939-1945
gptkbp:propulsion variable-pitch propeller
gptkbp:retired 1945
gptkbp:successor Kawasaki Ha-40
gptkbp:type radial engine
gptkbp:weight about 1,000 lbs