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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
passenger and cargo transport
twin-engine configuration
civil transport aircraft
100 kg/m²
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:crew
|
2
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|
gptkbp:design
|
gptkb:Hugo_Junkers
low-wing monoplane
|
|
gptkbp:engine
|
2
2 x 400 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1939
|
|
gptkbp:fuel_capacity
|
800 L
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|
gptkbp:height
|
3.5 m
|
|
gptkbp:historical_significance
|
used in World War II
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers A 260 B
|
|
gptkbp:influenced_by
|
gptkb:Junkers_F_13
|
|
gptkbp:is_used_by
|
gptkb:Luftwaffe
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
3,000 kg
|
|
gptkbp:notable_features
|
all-metal construction
|
|
gptkbp:notable_users
|
gptkb:German_Air_Force
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:operational_history
|
served in various roles during WWII
|
|
gptkbp:predecessor
|
gptkb:Junkers_A_50
|
|
gptkbp:production_location
|
gptkb:government_agency
|
|
gptkbp:production_years
|
1939-1945
|
|
gptkbp:propulsion
|
variable-pitch propeller
0.13 hp/kg
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
1945
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
8
1,000 kg
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
gptkb:1940
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Junkers_Ju_52
|
|
gptkbp:variant
|
gptkb:Junkers_A_260_A
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
15.5 m
|
|
gptkbp:bfsParent
|
gptkb:Junkers_A_260
|
|
gptkbp:bfsLayer
|
6
|