|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Curtiss_aircraft_family
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:item
1.8 m
2.1 m
6.5 m
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
enclosed
|
|
gptkbp:combat_role
|
transport and reconnaissance
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Don_Mc_Lean
|
|
gptkbp:engine
|
2
450 hp
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:first_flight
|
1937
two-pilot configuration
1937-06-30
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historical_significance
|
early transport aircraft development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss C-90 Condor
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
19.81 m
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
320 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
5,443 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:production_years
|
1937-1940
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,600 km
|
|
gptkbp:retired
|
1940s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:10
1,500 kg
|
|
gptkbp:service_ceiling
|
20,000 ft
6,100 m
|
|
gptkbp:speed
|
250 km/h
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:variant
|
C-90 A
C-90 B
|
|
gptkbp:wing_area
|
80.5 m²
|
|
gptkbp:wingspan
|
28.96 m
|