|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Curtiss_C-57
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Curtiss_C-46_Commando
manual flight control
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:aircraft
Curtiss engineers
|
|
gptkbp:engine
|
2
450 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
high aspect ratio wings
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
1,000 L
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historical_significance
|
early post-war transport aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-57 A
|
|
gptkbp:influences
|
post-war aircraft design
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
3,600 kg
|
|
gptkbp:navigation_system
|
radio navigation system
|
|
gptkbp:notable_features
|
large cabin space
|
|
gptkbp:operational_history
|
limited operational history
|
|
gptkbp:produced_by
|
50 units
|
|
gptkbp:production_years
|
1947-1950
|
|
gptkbp:propulsion
|
variable-pitch propellers
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
1950s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
1948
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Curtiss_C-57_B
|
|
gptkbp:variant
|
gptkb:Curtiss_C-57_B
|
|
gptkbp:weight
|
2,200 kg
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
15.85 m
|