|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_B97_M
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Mitsubishi_B97_M-2
civil aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
single aisle
tandem cockpit
|
|
gptkbp:combat_role
|
light transport
|
|
gptkbp:crew
|
2
|
|
gptkbp:date
|
post-war era
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
Mitsubishi engineers
|
|
gptkbp:developer
|
1945-1950
|
|
gptkbp:engine
|
2
300 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
high-wing configuration
|
|
gptkbp:first_flight
|
1950
successful
|
|
gptkbp:fuel_capacity
|
300 L
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historical_significance
|
first post-war aircraft by Mitsubishi
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B97 M-1
|
|
gptkbp:influences
|
American aircraft design
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:legacy
|
influenced future Mitsubishi designs
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
|
|
gptkbp:nickname
|
B97 M
|
|
gptkbp:notable_features
|
spacious cabin
|
|
gptkbp:operational_range
|
1,200 km
|
|
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
|
1,200 km
|
|
gptkbp:retirement_year
|
1960s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:services
|
1951
|
|
gptkbp:successor
|
gptkb:Mitsubishi_B97_M-2
|
|
gptkbp:variant
|
B97 M-2
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
12.0 m
|