|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_B33_M
|
|
gptkbp:aircraft_operated
|
gptkb:item
fixed-wing aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:capacity
|
10 passengers
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:date
|
1940s
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
high-wing monoplane
|
|
gptkbp:engine
|
2
300 hp
twin-engine
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1950
|
|
gptkbp:fuel_capacity
|
800 L
|
|
gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B33 M1
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
800 m
3,500 kg
|
|
gptkbp:origin
|
gptkb:Japan
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:produced_by
|
50
|
|
gptkbp:production_years
|
1950-1955
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
1960s
|
|
gptkbp:role
|
gptkb:aircraft
utility aircraft
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
1951
|
|
gptkbp:speed
|
250 km/h
|
|
gptkbp:successor
|
Mitsubishi B33 M2
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
Mitsubishi B33 M2
|
|
gptkbp:weight
|
2,200 kg
|
|
gptkbp:wingspan
|
20.0 m
|