|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:aircraft_operated
|
gptkb:Curtiss_C-46_Commando
gptkb:Charles_Lindbergh
cargo transport
high-wing
influenced future designs.
transport category aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
civilian transport
Curtiss design team
Curtiss engineers
|
|
gptkbp:developer
|
post-World War II era
|
|
gptkbp:engine
|
2
wing-mounted
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:first_flight
|
1947
various configurations
1947-06-01
|
|
gptkbp:fuel_capacity
|
1,500 liters
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historical_role
|
testing new technologies
|
|
gptkbp:historical_significance
|
early turboprop development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-80
|
|
gptkbp:influences
|
future transport aircraft designs
|
|
gptkbp:inspiration
|
C-46 Commando design
|
|
gptkbp:instrument
|
modern avionics for its time
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
6,350 kg
|
|
gptkbp:notable_features
|
high aspect ratio wings
|
|
gptkbp:number_built
|
gptkb:5
|
|
gptkbp:operational_history
|
limited operational history
|
|
gptkbp:primary_user
|
gptkb:aircraft
|
|
gptkbp:produced_by
|
limited production
|
|
gptkbp:production_years
|
1947-1948
|
|
gptkbp:range
|
1,600 km
|
|
gptkbp:retirement_year
|
1950
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:surface
|
elevators and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:wing_area
|
37.16 m²
|
|
gptkbp:wingspan
|
15.24 m
|