Middle East-ASIA
  Country
  Prime Manu.
  UAV Designation
Production status  
Operational status          
Power plants
Dimensions (m)            
  Wieghts (kg)  
        Performance      
  Comments
 Development
Production
Operation
 Purpose
Mission payload
Launch, take-off type
Recovery, landing type
Min crews need
System composite
Datalink, comm frequency
Engine
Propulsion
Wing span
Wing area (㎡)
Length overall
Height overall
Wheel track
Wheel base
Wing aspect ratio
Fuselage max width
Weight empty
Max fuel weight
Max Payload
Max T-O/launch weight
Max level speed (kt)
Cruising speed (kt)
Loiter speed (kt)
Stall speed (kt)
Service Ceiling (ft)
Max rate of climb (ft/min)
Range (nm)
Max Endurance (h)
Iran
HESA Qods
Ababil-B/ Ababil Ⅱ/ Ababil-S/ Ababil-T
Complete Underway Deployed  -B:Aerial target for Army defence units. -Ⅱ/S: Reconnaissance/ surveillance UAV. -T: Attack UAV Radar augmentation device(s) in Ababil-B; small camera in Ababil Ⅱ; EO camera in Ababil-S; Daylight TV sensor and HE warhead in Ababil-T.  Pneumatic launcher of HESA; booster rocket. Launchable from land or ship's deck. Belly skid landing or HESA cruciform parachute.      Real-time imagery downlink in Ababil-S. One P 73 rotary piston engine. Two-blade pusher prop. 3.33   2.80 0.935               83 200/ 162 16/ 65/ 81/ 27     10,820/ 14,000        
First flight :-Ⅱ in October 1997.                                                          
Mohadjer 2/ Mohadjer 3/ Mohadjer 4
Complete Underway Deployed Multirole UAV family. 2/3 : video camera; 4: IR camera/ ECM. PL3 pneumatic catapult, booster rocket, conventional wheeled take-off. Parachute recovery, skid or wheeled landing.       Single flat-twin piston engine. Two-blade pusher prop. 3.80    2.879 1.03         70       108       11,000   27/ 54/ 81 1.5/ 3/ 7  
                                                               
Talash 1/ Talash 2
Complete Underway Deployed Operator training UAV and decoy. -2: ECM Conventional wheeled take-off (Talash 1). Rail launch by pneumatic catapult or booster rocket (Talash 2).  Cnoventional wheeled landing (T-1). Parachute recovery system or belly skid landing (T-2).       Single- cylinder piston engine. Two-blade tractor prop.  2.64/ 2.10   1.70/ 1090                  12/ 11  48/ 65            50 m/ 80 m 30 min/ 25 min  
                                                                 
IRAQ
FSPF
L-29
Complete     Attack UAV    Conventional runway take-off.  Conventional runway lnading.       One 1,962 lb st Motorlet M 701c-500 turbojet.   10.29    10.81  3.31          2,280  1,050 liters + two 15 liter auxiliary fuel tanks   3,280/ 3,540 332     87 36,000  2,755 344/ 480 1.0 Standard L-29 spec
                                                                 
  Country
  Prime Manu.
  UAV Designation
Production status  
Operational status          
Power plants
Dimensions (m)            
  Wieghts (kg)  
        Performance      
  Comments
 Development
Production
Operation
 Purpose
Mission payload
Launch, take-off type
Recovery, landing type
Min crews need
System composite
Datalink, comm frequency
Engine
Propulsion
Wing span
Wing area (㎡)
Length overall
Height overall
Wheel track
Wheel base
Wing aspect ratio
Fuselage max width
Weight empty
Max fuel weight
Max Payload
Max T-O/launch weight
Max level speed (kt)
Cruising speed (kt)
Loiter speed (kt)
Stall speed (kt)
Service Ceiling (ft)
Max rate of climb (ft/min)
Range (nm)
Max Endurance (h)
Turkey
EES
Kanarya
Complete  Underway    Close-range UAV    Wheeled take-off; launcher optional. Wheeled landing; parachute optional.  2     Twin piston engines Two-blade pusher prop  4.40   2.57               20 80 100       15,000   54 8.0  
     Available to order                                                        
Kirlangic
Complete Underway Deployed Improved version of EAS Crow; CR    Wheeled take-off; launcher optional. Wheeled landing; parachute optional. 3     Twin piston engines Two-blade pusher prop 5.30   3.10               32 145 100       22,600   81 16  
    In service                                                      
Doğan
Complete Underway Deployed Drived from EAS Vanguard; SR    Wheeled take-off; launcher optional. Wheeled landing; parachute optional. 3     Twin piston engines Two-blade pusher prop 6.60   3.70               60 200 110       24,000   108 19  
    In service                                                      
Serce
Complete Underway   Midium-range UAV   Wheeled take-off Wheeled landing 3     Twin piston engines Two-blade pusher prop 9.00   5.05               100 385 120       26,000   135 32  
    Available to order                                                        
Sahin
Complete Underway   Long-range Long-endurance UAV   Wheeled take-off Wheeled landing 3     Twin piston engines Two-blade pusher prop 13.20   7.40               200 825 120       26,000   216 40  
    Available to order                                                        
TAI (Turkey Aerospace Industries Ins)
UAV-X1
Complete(?) Underway Deployed(?) Short-range surveillance UAV             One 42 hp UEL AR 801 rotary engine. A three-blade pusher prop 6.00 6.00 4.00 1.92       0.40 150 40 30 245 120 100 70 45 15,000 500 644 7h 36 min  
Since 1989, and the first flight was made on 19 October 1992. Turkish Ministry of National Defence   Wheeled take-off Wheeled landing                                                
  Country
  Prime Manu.
  UAV Designation
Production status  
Operational status          
Power plants
Dimensions (m)            
  Wieghts (kg)  
        Performance      
  Comments
 Development
Production
Operation
 Purpose
Mission payload
Launch, take-off type
Recovery, landing type
Min crews need
System composite
Datalink, comm frequency
Engine
Propulsion
Wing span
Wing area (㎡)
Length overall
Height overall
Wheel track
Wheel base
Wing aspect ratio
Fuselage max width
Weight empty
Max fuel weight
Max Payload
Max T-O/launch weight
Max level speed (kt)
Cruising speed (kt)
Loiter speed (kt)
Stall speed (kt)
Service Ceiling (ft)
Max rate of climb (ft/min)
Range (nm)
Max Endurance (h)
UAE
AES
Nibbio 1
Complete  Underway Deployed Multirole UAV Modular design permits carriage of sensors for reconnaissance, surveillance, target acquisition, anti-radar missions, EW or communication relay.  Conventional wheeled take-off or with booster rocket assistance.  Conventional wheeled lnading. Parachute for emergency recovery.       One 45 hp AES AE 626 flat-twin two-stroke engine Two-blade pusher prop 5.60   5.10 1.10         102   55 240 136 97     19,680  1,772 >108 10  
    Servicing in UAE armed forces.                                                        
Nibbio 2
Complete Underway Deployed Export version. Less advanced avionics than Mibbio 1.                                                        
   Two systems delivered to an unidentified customer in 1999.