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gptkbp:instance_of
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gptkb:unmanned_aerial_vehicle
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|
gptkbp:combat_radius
|
up to 1,000 km
|
|
gptkbp:communication_system
|
satellite communication
|
|
gptkbp:data_link_range
|
250 km
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|
gptkbp:elevation
|
up to 30,000 feet
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|
gptkbp:endurance
|
over 52 hours
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gptkbp:engine_type
|
gptkb:diesel_engine
|
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gptkbp:exported_to
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gptkb:Australia
gptkb:Brazil
gptkb:Canada
gptkb:Germany
gptkb:India
gptkb:Singapore
gptkb:Turkey
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gptkbp:first_flight
|
gptkb:2005
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Heron Mk I
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gptkbp:is_monitored_by
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electro-optical/infrared sensors
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gptkbp:launch_window
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gptkb:catapult
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|
gptkbp:length
|
8.5 meters
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|
gptkbp:manufacturer
|
gptkb:Israel_Aerospace_Industries
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:navigation_system
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gptkb:GPS
|
|
gptkbp:notable_features
|
high availability
modular design
real-time data transmission
user-friendly interface
multi-mission capability
advanced avionics
high reliability
high altitude capability
advanced sensor suite
easy maintenance
low operational costs
secure communication links
real-time video feed
environmental adaptability
autonomous flight capabilities
long endurance
data fusion capabilities
high payload flexibility
modular payloads
stealthy design
high endurance missions
intelligent mission planning
advanced ground control station
high data processing power
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|
gptkbp:payload_capacity
|
up to 350 kg
|
|
gptkbp:primary_user
|
gptkb:Israel_Defense_Forces
|
|
gptkbp:production_status
|
in service
|
|
gptkbp:recovery_method
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gptkb:parachute
|
|
gptkbp:role
|
intelligence, surveillance, and reconnaissance
|
|
gptkbp:service_ceiling
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gptkb:10,000_meters
|
|
gptkbp:variant
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gptkb:Heron_TP
|
|
gptkbp:wingspan
|
16.6 meters
|
|
gptkbp:bfsParent
|
gptkb:De_Havilland_Heron
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|
gptkbp:bfsLayer
|
6
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