gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
military aircraft
single-engine
trainer aircraft
high-wing
basic trainer
|
gptkbp:armament
|
none
|
gptkbp:cockpit
|
open cockpit
|
gptkbp:constructionMaterial
|
metal
fabric-covered wood
|
gptkbp:controls
|
elevator, ailerons, rudder
|
gptkbp:crew
|
2
basic flight training
|
gptkbp:decommissioned
|
1945
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
1938-1940
low wing loading
|
gptkbp:engineType
|
piston engine
|
gptkbp:firstFlight
|
1940
1945
|
gptkbp:fuelCapacity
|
200 liters
|
gptkbp:height
|
2.8 m
|
gptkbp:historicalSignificance
|
used_in_World_War_II
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi M-50
|
gptkbp:influencedBy
|
Mitsubishi Ki-15
|
gptkbp:landingGear
|
tailwheel
|
gptkbp:length
|
8.5 m
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
gptkbp:maxSpeed
|
300 km/h
|
gptkbp:maxTakeoffWeight
|
1,600 kg
|
gptkbp:nickname
|
gptkb:Mitsubishi_Trainer
|
gptkbp:numberOfEpisodes
|
1
|
gptkbp:operationalHistory
|
served in training roles
|
gptkbp:participatesIn
|
training pilots
|
gptkbp:primaryUser
|
gptkb:Japanese_military
|
gptkbp:productionLocation
|
gptkb:Japan
|
gptkbp:productionYears
|
1940-1945
|
gptkbp:propulsion
|
two-bladed propeller
|
gptkbp:range
|
1,000 km
|
gptkbp:relatedAircraft
|
gptkb:Mitsubishi_M-6A
|
gptkbp:role
|
military trainer
|
gptkbp:services
|
6,000 m
|
gptkbp:successor
|
gptkb:Mitsubishi_M-6A
|
gptkbp:takeoffDistance
|
300 m
400 m
|
gptkbp:totalGoals
|
approximately 100
|
gptkbp:usedBy
|
gptkb:Imperial_Japanese_Army_Air_Service
|
gptkbp:variant
|
M-50A
M-50B
|
gptkbp:weight
|
1,200 kg
|
gptkbp:wingspan
|
10.5 m
|