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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
7
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gptkbp:bfsParent
|
gptkb:Mitsubishi_B26_M
gptkb:Mitsubishi_B45_M
gptkb:Mitsubishi_B50_M
gptkb:Mitsubishi_B53_M
|
|
gptkbp:aircraft_operated
|
gptkb:Mitsubishi_A6_M_Zero
gptkb:Mitsubishi_T-2
gptkb:Mitsubishi_Ki-15
gptkb:item
low-wing
military trainer
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
basic trainer
|
|
gptkbp:engine
|
gptkb:musical
single-engine
250 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
control stick
|
|
gptkbp:fuel_capacity
|
200 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi Ha-211
|
|
gptkbp:influenced_by
|
gptkb:Mitsubishi_Ki-51
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
retractable
tricycle gear
|
|
gptkbp:length
|
8.3 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
tandem seating arrangement
|
|
gptkbp:number_built
|
gptkb:television_series
|
|
gptkbp:operational_history
|
used in training missions
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:production_years
|
1956-1962
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
8,000 m
|
|
gptkbp:services
|
gptkb:1956
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Mitsubishi_T-2
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
Mitsubishi Ha-211 A
Mitsubishi Ha-211 B
|
|
gptkbp:wingspan
|
10.5 m
|