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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:ceiling
|
8,000 m
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
open cockpit
single-seat
|
|
gptkbp:control_surfaces
|
gptkb:elevator
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:France
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
Marcel Caudron
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1946
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Caudron C.720
|
|
gptkbp:influenced_by
|
gptkb:Caudron_C.640
gptkb:Caudron_C.710
Caudron C.635
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Caudron
|
|
gptkbp:max_speed
|
600 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
high speed
agility
lightweight design
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:produces
|
50
limited
|
|
gptkbp:production_years
|
1946-1949
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:retirement
|
1950s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
gptkb:fighter_aircraft
|
|
gptkbp:service_entry
|
1947
|
|
gptkbp:stall_speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Caudron_C.740
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:used_by
|
gptkb:French_Air_Force
civil operators
|
|
gptkbp:variant
|
Caudron C.720 A
Caudron C.720 B
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wing_configuration
|
low-wing
|
|
gptkbp:wingspan
|
9.5 m
|
|
gptkbp:bfsParent
|
gptkb:Caudron_C.450
|
|
gptkbp:bfsLayer
|
7
|