|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:communicationEquipment
|
data link
|
|
gptkbp:constructionMaterial
|
composite materials
|
|
gptkbp:defeated
|
multiple nations
|
|
gptkbp:developer
|
gptkb:Elbit_Systems
|
|
gptkbp:electrification
|
diesel engine
|
|
gptkbp:endurance
|
up to 20 hours
|
|
gptkbp:engineType
|
rotary engine
|
|
gptkbp:exportedTo
|
various countries
|
|
gptkbp:firstFlight
|
2007
|
|
gptkbp:homeGround
|
required for operations
mobile or fixed
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Elbit Systems Hermes 450
|
|
gptkbp:launchSite
|
catapult
|
|
gptkbp:length
|
8.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Elbit_Systems
|
|
gptkbp:maxTakeoffWeight
|
450 kg
|
|
gptkbp:missions
|
autonomous
|
|
gptkbp:navigationEquipment
|
gptkb:GPS
|
|
gptkbp:notableFeature
|
high endurance
real-time data transmission
multi-mission capability
low radar cross-section
high altitude operation
|
|
gptkbp:offers
|
approximately $2 million
|
|
gptkbp:operationalStatus
|
2007
up to 15,000 feet
all weather
|
|
gptkbp:passenger_traffic
|
modular
various sensors
|
|
gptkbp:payloadCapacity
|
150 kg
|
|
gptkbp:priceRange
|
up to 200 km
|
|
gptkbp:primaryUser
|
military
civilian
|
|
gptkbp:renovated
|
parachute
|
|
gptkbp:role
|
intelligence, surveillance, reconnaissance
|
|
gptkbp:sensors
|
infrared
radar
electro-optical
|
|
gptkbp:speed
|
120 knots
|
|
gptkbp:successor
|
gptkb:Hermes_900
|
|
gptkbp:supportRole
|
used in various conflicts
|
|
gptkbp:surveillanceEquipment
|
up to 150 km
|
|
gptkbp:takeoffDistance
|
200 meters
150 meters
|
|
gptkbp:training
|
required for operators
|
|
gptkbp:wingspan
|
14 meters
|