Mitsubishi M-17

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instanceOf aircraft
gptkbp:aircraft air superiority
single-engine
low-wing
gptkbp:armament machine guns
bombs
gptkbp:cockpit enclosed
gptkbp:constructionMaterial metal
gptkbp:crew 1
required
gptkbp:design gptkb:Mitsubishi_Aircraft_Company
1930s
streamlined fuselage
Mitsubishi_engineers
gptkbp:engine gptkb:Mitsubishi_Kasei
gptkbp:enginePower 1,000 hp
gptkbp:firstFlight 1937
1945
gptkbp:floors tailplane
gptkbp:fuelCapacity 500 liters
gptkbp:headlights conventional tail
gptkbp:historicalSignificance early WWII fighter
https://www.w3.org/2000/01/rdf-schema#label Mitsubishi M-17
gptkbp:influenced later_Japanese_fighters
gptkbp:influencedBy gptkb:Mitsubishi_A5M
gptkbp:landingGear tricycle gear
gptkbp:length 9.0 m
gptkbp:manufacturer gptkb:Mitsubishi
gptkbp:maxSpeed 500 km/h
gptkbp:maxTakeoffWeight 3,000 kg
gptkbp:nationalTeam gptkb:Japan
gptkbp:numberBuilt approximately 100
gptkbp:operationalRange 1,000 km
gptkbp:operationalStatus wing flaps
gptkbp:produces limited
gptkbp:productionYears 1937
gptkbp:propulsion variable pitch
gptkbp:retirementYear 1945
gptkbp:role fighter aircraft
interceptor
gptkbp:service_ceiling 10,000 m
gptkbp:serviceHistory limited combat use
gptkbp:services 1937-1945
gptkbp:setting monoplane
gptkbp:speed 80 km/h
gptkbp:steering vertical stabilizer
gptkbp:succeededBy 5°/s
gptkbp:successor Mitsubishi J2M
gptkbp:supportRole gptkb:World_War_II
1938
defense
gptkbp:takeoffDistance 100 km/h
gptkbp:usedBy gptkb:Imperial_Japanese_Army_Air_Service
gptkbp:variant M-17A
gptkbp:wingArea 30 m²
gptkbp:wingspan 12.0 m