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Hermes 900 Israeli Unmanned Aerial Vehicle (UAV)

Multirole Fighter Aircraft
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Basic Information
Name
Hermes 900 Israeli Unmanned Aerial Vehicle (UAV)
Designation
Alternate Designation
Equipment Type
Multirole Fighter Aircraft
Manufacturer
Elbit Systems
Date of Introduction
2012
Description

The Elbit Systems Hermes 900 Kochav (Star) is an Israeli medium-size, multi-payload, medium-altitude long-endurance unmanned aerial vehicle (UAV) designed for tactical missions. It is a sequel to the Hermes 450 series of drones, one of the most widely used military drones in the world. It has an endurance of up to 30 hours with a service ceiling of 30,000 feet (9,100 m). Its primary mission is reconnaissance, surveillance, and communications relay. The Hermes 900 has a wingspan of 15 m (49 ft) and weighs 970 kg (2,140 lb), with a payload capability of 300 kg (660 lb). Payload options include electro-optical/infrared sensors, synthetic-aperture radar/ground-moving target indication, communications and electronic intelligence, electronic warfare, and hyperspectral sensors.

Air & Air Defense Specifications
Engine Turbocharged Gasoline Engine (105 hp)
Variants
Hermes 900, Attack Version An attack version of Hermes 900 may be possible. Each wing has two external hardpoints similar to the weaponized Hermes 450. The Mikholit, Israeli 10km variant of Nimrod long-range missile, is designed for launch from the Hermes 450.
System
Alternative designations Hermes 900 Israeli Unmanned Aerial Vehicle (UAV)
Type Medium-Altitude Long-Endurance Unmanned Aerial Vehicle (UAV)
Manufacturer Elbit Systems
Ground Crew 2 ea
Cruising Speed 112 km/h (70 mph, 60 kn)
Maximum Speed 220 km/h (140 mph, 120 kn)
Endurance 30 hrs
Ceiling, Service 9,100 m (30,000 ft)
Radius of Operation 1,000 km
Launch Method Wheeled take-off
Recovery Method Conventional landing
Landing Method 3-wheeled, retractable landing gear. independent take-off and landing
Flight Control Method Preprogrammed/in-flight reprogram. Secure redundant Line of Sight data link and redundant satellite communications beyond line of sight
Flight Control Ground control station vehicle. can control two Hermes simultaneously
Dimensions
Length 6.1 m
Wing Span 15.3 m
Overall Height 2.36 m
Take-off Weight 970 kg
Payload 300 kg
Automotive
Engine Name Rotax 914
Engine Type Turbocharged Gasoline Engine
Engine Power 105 hp
Propeller 3-blade pusher/puller
Launch and Recovery
Landing Method Conventional landing
Launch Method Wheeled take-off
Recovery/Landing Method 3-wheeled, retractable landing gear.
Wind speed at launch INA
Payload Types
Gabbiano T200 - Synthetic Aperture Radar
Description Long range surveillance radar, x band (8-12.5 GHz), 407km maritime range, MTI and SAr, >200 target Track-While Scan (TWS)
Moving Target Indication Yes
DSP-1 Electro Optical Camera
Description Camera
Detection Range 25 km
Recognition Range 10 km
Swath 400 ha
FLIR Enabled Yes
Laser Designator Yes
Tadiran SKYFIX / SKYJAM EW Payload
Intecept Freq. range 20 - 500 MHz
Direction Finding Freq. Range 1.5 - 1000 MHz
Jammer Freq. Range 20 - 500 MHz
Emerald AES-210V
Description ELINT
Elop DCoMPASS
Description Digital compact multi-purpose advanced stabilized system. Stabilized turret incorporating thermal imager, color TV, dual-band laser designator rangefinder, inertial measurement unit and laser spot tracker
Survivability / Countermeasures
Description A light composite structure, low radar signature.
Details
Country of Origin Israel
Category UAVs
Air > UAVs
Filter Label
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
6.1 m
Width
Height
2.36 m
Weight
970 kg
Operators (9)
Israel
Brazil
Azerbaijan
Chile
Colombia
Iceland
Mexico
Switzerland
Thailand
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