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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Curtiss's_aircraft
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Curtiss_transport_aircraft
gptkb:item
cargo transport
cantilever wing
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
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|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
1950s
|
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gptkbp:design
|
Curtiss engineers
|
|
gptkbp:engine
|
1,200 hp
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:features
|
large cargo door
|
|
gptkbp:first_flight
|
1939
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|
gptkbp:fuel_capacity
|
1,200 liters
|
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gptkbp:historical_significance
|
gptkb:Company
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-52
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
90 km/h
120 km/h
3,600 kg
|
|
gptkbp:military_technology
|
logistics support
|
|
gptkbp:nickname
|
gptkb:C-52_Commando
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:origin
|
gptkb:USA
|
|
gptkbp:primary_user
|
gptkb:USAAF
|
|
gptkbp:production_location
|
gptkb:USA
|
|
gptkbp:production_years
|
1939-1942
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:replaced_by
|
gptkb:C-130_Hercules
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
1,500 kg
2+6 seating arrangement
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
gptkb:1940
1940-1950s
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:successor
|
gptkb:Curtiss_C-54
|
|
gptkbp:tail_type
|
gptkb:item
T-tail
|
|
gptkbp:variant
|
gptkb:C-52_A
C-52 B
|
|
gptkbp:wingspan
|
16.5 m
|