Mitsubishi Ha-102

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:compression_ratio 6.5:1
gptkbp:configuration V-type
gptkbp:cooling_system liquid-cooled
water-cooled
gptkbp:country_of_origin gptkb:Japan
gptkbp:displacement 1,800 cc
gptkbp:engine gptkb:military_aircraft
limited production
advanced features for its time
influenced future engine designs
faced production challenges
used in several aircraft types
incorporated innovative technologies
recognized for its engineering excellence
developed during World War II
developed by Mitsubishi Heavy Industries
historically significant in aviation history
gptkbp:engine_configuration air-cooled
detailed specifications available
V-12 configuration
characteristics suitable for combat aircraft
specifications published in aviation journals
V-engine layout
focused on power and efficiency
gptkbp:engine_displacement 1,800 cc
gptkbp:engine_power 1,000 hp
high reliability
excellent performance
2,500 RPM
performance compared favorably to contemporaries
gptkbp:engine_production_numbers limited production numbers due to war.
gptkbp:engine_type no known variants
V-12 engine
gptkbp:first_flight gptkb:1944
gptkbp:fuel_capacity 400 kg
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Mitsubishi Ha-102
gptkbp:impact significant impact on Japanese aviation
gptkbp:is_tested_for extensively tested
gptkbp:manufacturer gptkb:Mitsubishi
gptkbp:notable_feature high power-to-weight ratio
gptkbp:number_of_engines gptkb:12
gptkbp:power_output 1,000 hp
gptkbp:production_years 1944-1945
gptkbp:propeller variable-pitch propeller
gptkbp:related_aircraft gptkb:Mitsubishi_A6_M_Zero
gptkb:Mitsubishi_G4_M
gptkbp:successor gptkb:Mitsubishi_Ha-211
gptkbp:torque 1,200 Nm
gptkbp:type piston engine
gptkbp:used_in gptkb:Mitsubishi_J2_M_Raiden
gptkbp:valve_configuration overhead valve
gptkbp:weight 400 kg
gptkbp:bfsParent gptkb:Mitsubishi_Ha-101
gptkbp:bfsLayer 7