|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Junkers_A_240
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Junkers_Ju_52
cargo and passenger transport
civil and military
high-wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
8:1
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:date
|
1938
|
|
gptkbp:design
|
gptkb:Hugo_Junkers
|
|
gptkbp:engine
|
2
1,200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
all-metal construction
|
|
gptkbp:first_flight
|
1939
1939-05-01
|
|
gptkbp:fuel_capacity
|
1,200 L
|
|
gptkbp:height
|
4.5 m
|
|
gptkbp:historical_significance
|
used in military operations during WWII
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers A 240 A
|
|
gptkbp:is_used_by
|
gptkb:Luftwaffe
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:material
|
15.5 m
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
3,500 kg
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_area
|
civil and military aviation
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:origin
|
gptkb:government_agency
|
|
gptkbp:power_output
|
gptkb:Junkers_Jumo_211
|
|
gptkbp:production_location
|
gptkb:government_agency
|
|
gptkbp:production_years
|
1939-1945
|
|
gptkbp:propulsion
|
variable-pitch propellers
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retirement_year
|
gptkb:Company
1945
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:12
1,500 kg
1,000 kg
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Junkers_Ju_252
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
50 m²
|
|
gptkbp:wingspan
|
20.0 m
|