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Yabhon-R  
Initial Operational Capability (IOC): 2010
Total Production: ?
Origin: United Arab Emirates
Corporations: ADCOM Systems
Parent System: Yabhon-R
Initial Operational Capability (IOC): 2010
Total Production: ?
Family Members: Yabhon-R2
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Description: The ADCOM Systems Yabhon-R is a medium altitude, long endurance (MALE) unmanned aircraft system (UAS) designed to carry out missions including: real time day/night intelligence, reconnaissance and surveillance (ISR), search and rescue (SAR), border surveillance and remote area monitoring. The delta-canard wing aircraft is powered by a single 100-hp engine driving a three-blade propelled at the tail. This configuration allows a cruise speed of 240 kilometers per hour and a flight endurance of 27 hours. The Yabhon-R has been optimized for operations from short and unprepared runways with emergency landing using a built-in parachute. The payload includes electro-optical sensors such as thermal imager, TV camera, laser range finder and laser designator. The landing wheels are fixed expect the nose wheel which is retractable.

Yabhon-R Specifications

Crew: 0
Number of Engines: 1
Propeller Blades: 3
Area
Wing Area: 8 square meter (86 square foot)
Dimensions
Height: 2 meter (6.56 foot)
Length: 5 meter (16.4 foot)
Wingspan: 6.50 meter (21.3 foot)
Performance
Ceiling: 6,700 meter (21,982 foot)
Power
Max Power at TakeOff: 100 hp (75 kW)
Speed
Cruise Speed: 240 kph (149 mph)
Stall Speed: 92 kph (50 knot)
Time
Flight Endurance: 27 hour (1.13 day)
Volume
Fuel Tank Capacity: 240 liter
Weight
Empty Weight: 270 kilogram (595 pound)
Max Takeoff Weight: 570 kilogram (1,257 pound)
Payload: 120 kilogram (265 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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