|
gptkbp:instance_of
|
gptkb:unmanned_aerial_vehicle
|
|
gptkbp:ceiling
|
6000 meters
|
|
gptkbp:communication_system
|
gptkb:radio_station
|
|
gptkbp:control_system
|
gptkb:remote_control
|
|
gptkbp:decommissioned
|
1990s
|
|
gptkbp:design
|
fixed-wing
Thomson-CSF engineers
|
|
gptkbp:development
|
1960s to 1970s
|
|
gptkbp:elevation
|
3000 meters
|
|
gptkbp:endurance
|
24 hours
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
100 liters
|
|
gptkbp:fuselage_material
|
aluminum
|
|
gptkbp:home_ground
|
mobile unit
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Thomson-CSF Cyrano IV
|
|
gptkbp:is_monitored_by
|
day and night
|
|
gptkbp:launch_site
|
gptkb:military_base
|
|
gptkbp:launch_window
|
gptkb:catapult
|
|
gptkbp:legacy
|
pioneering UAV technology
|
|
gptkbp:length
|
8.5 meters
|
|
gptkbp:manufacturer
|
Thomson-CSF
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:navigation_system
|
gptkb:GPS
|
|
gptkbp:notable_features
|
autonomous flight
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_range
|
1000 km
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:payload_capacity
|
gptkb:camera
|
|
gptkbp:price
|
1 million USD
|
|
gptkbp:production_status
|
retired
|
|
gptkbp:provides_information_on
|
encrypted
|
|
gptkbp:recovery_method
|
gptkb:parachute
|
|
gptkbp:related_model
|
Cyrano I
|
|
gptkbp:retirement
|
advancements in technology
|
|
gptkbp:role
|
reconnaissance
|
|
gptkbp:success_rate
|
high
|
|
gptkbp:successor
|
Cyrano II
|
|
gptkbp:target_market
|
gptkb:military
|
|
gptkbp:training
|
gptkb:military_personnel
|
|
gptkbp:used_by
|
French military
|
|
gptkbp:user_countries
|
gptkb:none
|
|
gptkbp:weight
|
500 kg
|
|
gptkbp:wingspan
|
14 meters
|
|
gptkbp:bfsParent
|
gptkb:Mirage_F1_B
gptkb:Mirage_F1_E
|
|
gptkbp:bfsLayer
|
6
|