gptkbp:instance_of
|
gptkb:aircraft
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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-70
general aviation
retired
utility aircraft
high-wing monoplane
good maneuverability
paved the way for future designs.
|
gptkbp:avionics
|
basic navigation instruments
|
gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
two-seat cockpit
|
gptkbp:combat_role
|
light transport
|
gptkbp:constructed_in
|
50
|
gptkbp:crew
|
2
|
gptkbp:date
|
1940s
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
|
gptkbp:engine
|
2
250 hp
piston engine configuration
|
gptkbp:engine_type
|
piston engine
|
gptkbp:features
|
all-metal construction
|
gptkbp:first_flight
|
1950
|
gptkbp:fuel_capacity
|
800 L
|
gptkbp:historical_significance
|
first post-war Japanese aircraft
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B9 M
|
gptkbp:influenced_by
|
gptkb:Mitsubishi_Ki-46
|
gptkbp:inspiration
|
post-war aviation needs in Japan
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
12.5 m
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
gptkbp:material
|
aluminum alloy
|
gptkbp:max_speed
|
300 km/h
|
gptkbp:max_takeoff_weight
|
3,500 kg
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
gptkbp:operational_history
|
used in various civil roles
|
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:10
|
gptkbp:service_ceiling
|
6,000 m
|
gptkbp:services
|
1951
|
gptkbp:setting
|
high-wing
|
gptkbp:successor
|
gptkb:Mitsubishi_B-70
|
gptkbp:tail_type
|
T-tail
|
gptkbp:weight
|
2,200 kg
|
gptkbp:wing_area
|
30 m²
|
gptkbp:wingspan
|
15.5 m
|