|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aired_on
|
gptkb:none
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
7.0
|
|
gptkbp:climb_rate
|
6 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:control_surfaces
|
ailerons
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:Mitsubishi_Kasei_14
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:financial_stability
|
fin
|
|
gptkbp:first_flight
|
gptkb:1954
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
conventional tail
|
|
gptkbp:fuel_capacity
|
500 L
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
2.80 m
|
|
gptkbp:historical_significance
|
first indigenous jet trainer in Japan
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi 104 A
|
|
gptkbp:introduced
|
gptkb:1954
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.53 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
2,500 kg
|
|
gptkbp:notable_pilots
|
gptkb:Mitsubishi_test_pilots
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
used for training purposes.
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:production_location
|
gptkb:Japan
|
|
gptkbp:production_years
|
1954-1958
|
|
gptkbp:propeller
|
two-bladed propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:related_aircraft
|
Mitsubishi 100 A
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service_ceiling
|
5,500 m
|
|
gptkbp:stall_speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Mitsubishi_T-2
|
|
gptkbp:tailplane
|
horizontal stabilizer
|
|
gptkbp:variant
|
gptkb:Mitsubishi_104_B
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wing_configuration
|
gptkb:metal
|
|
gptkbp:wingspan
|
10.92 m
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_104_B
|
|
gptkbp:bfsLayer
|
7
|