|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Giovanni_Battista_Caproni
|
|
gptkbp:aircraft_operated
|
gptkb:Caproni_Ca.335
gptkb:Caproni_Ca.310
hydraulic control system
|
|
gptkbp:armament
|
gptkb:rocket
machine guns
|
|
gptkbp:casualties
|
gptkb:none
|
|
gptkbp:cockpit
|
pressurized cockpit
tandem seating
|
|
gptkbp:crew
|
gptkb:3
|
|
gptkbp:date
|
gptkb:1942
|
|
gptkbp:design
|
gptkb:Giovanni_Battista_Caproni
multirole capabilities
Caproni design team
|
|
gptkbp:emergency_services
|
parachute escape system
|
|
gptkbp:engine
|
1200 hp
Caproni V-12
|
|
gptkbp:engine_type
|
liquid-cooled
|
|
gptkbp:features
|
high wing configuration
|
|
gptkbp:first_flight
|
1943
|
|
gptkbp:fuel_capacity
|
2000 L
|
|
gptkbp:historical_context
|
Axis powers aircraft
|
|
gptkbp:historical_significance
|
World War II aircraft development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Caproni Ca.2600
|
|
gptkbp:influences
|
post-war aircraft design
Italian aviation design
|
|
gptkbp:landing_gear
|
gptkb:horse_race
|
|
gptkbp:length
|
20.5 m
|
|
gptkbp:manufacturer
|
gptkb:Caproni
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
8000 kg
800 m
|
|
gptkbp:navigation_system
|
radio navigation
|
|
gptkbp:number_built
|
gptkb:10
|
|
gptkbp:operational_area
|
gptkb:none
|
|
gptkbp:origin
|
gptkb:Italy
|
|
gptkbp:produced_by
|
limited production
|
|
gptkbp:production_years
|
1943-1944
|
|
gptkbp:propulsion
|
twin-engine
|
|
gptkbp:range
|
1000 km
|
|
gptkbp:role
|
strategic bombing
|
|
gptkbp:service_ceiling
|
8000 m
|
|
gptkbp:status
|
gptkb:patent
|
|
gptkbp:surface
|
elevators
ailerons
rudder
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
Ca.2601
|
|
gptkbp:wing_area
|
70 m²
|
|
gptkbp:wingspan
|
22.0 m
|