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NRUAV  
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: Naval Rotary UAV
Origin: Israel
Corporations: Israel Aerospace Industries Ltd. (IAI)
Parent System: NRUAV
Initial Operational Capability (IOC):
Total Production: ?
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Description: The IAI Naval Rotary UAV (NRUAV) is a tactical unmanned rotorcraft designed to provide over the horizon targeting (OTHT), real-time battle damage assessment (BDA) and intelligence, surveillance and reconnaissance (ISR) missions. It is based on IAI's Malat-made Helicopter Modification Suite (HeMoS) platform. The NRUAV features automatic take-off and landing (ATOL) from warships and fully redundant system. It is equipped with a line-of-sight data link and can accommodate a variety of payloads such as electro-optical sensors, multi-mode radars, electronic support measures (ESM) or Communications Intelligence (COMINT) payload. The NRUAV can remain on station for six hours at ranges of 150 kilometers carrying a 220 kg payload.

NRUAV Specifications

Crew: 0
Main Rotor Blades: 3
Tail Rotor Blades: 2
Dimensions
Height: 2.97 meter (9.74 foot)
Length: 12.8 meter (42 foot)
Main Rotor Diameter: 11.0 meter
Tail Rotor Diameter: 1.91 meter
Performance
Ceiling: 15,000 foot (4,572 meter)
Max Range: 150 kilometer (81 nautical mile)
Speed
Loiter Speed: 60 knot (111 kph)
Top Speed at High Altitude: 100 knot (185 kph)
Time
Flight Endurance: 6 hour (0.25 day)
Weight
Max Takeoff Weight: 2,200 kilogram (4,850 pound)
Payload: 220 kilogram (485 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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