gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Mitsubishi_Type_13
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gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Mitsubishi_B-67
cantilever wing
|
gptkbp:armament
|
gptkb:none
|
gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
pressurized
|
gptkbp:crew
|
gptkb:3
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
gptkb:public_transportation_system
|
gptkbp:engine
|
2
450 hp
|
gptkbp:engine_type
|
gptkb:Mitsubishi_Ha-211
piston engine
|
gptkbp:features
|
high aspect ratio wings
spacious cabin
large cargo door
|
gptkbp:first_flight
|
1950
|
gptkbp:fuel_capacity
|
3,000 liters
|
gptkbp:historical_significance
|
first post-war transport aircraft in Japan
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B45 M
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
22.5 m
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
gptkbp:material
|
monocoque
|
gptkbp:max_speed
|
400 km/h
|
gptkbp:max_takeoff_weight
|
80 km/h
6,000 kg
|
gptkbp:number_built
|
50
|
gptkbp:operational_range
|
1,200 km
|
gptkbp:origin
|
gptkb:Japan
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
gptkbp:production_years
|
1950-1955
|
gptkbp:propulsion
|
variable-pitch propeller
|
gptkbp:range
|
1,500 km
|
gptkbp:retirement_year
|
1960s
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:seating_capacity
|
gptkb:television_series
1,500 kg
|
gptkbp:service_ceiling
|
6,000 m
|
gptkbp:services
|
1951
1951-1960s
|
gptkbp:setting
|
high-wing monoplane
|
gptkbp:successor
|
gptkb:Mitsubishi_B-67
|
gptkbp:surface
|
elevators
ailerons
rudder
|
gptkbp:tail_type
|
T-tail
|
gptkbp:variant
|
gptkb:Mitsubishi_B45_M-1
|
gptkbp:wing_area
|
80 m²
|
gptkbp:wingspan
|
30.0 m
|