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Military


Ababil (Swallow) Unmanned Air Vehicle


Specifications
wing span 325 cm
wing airfoil section NACA-4412
wing area 1.76m2
canard span 168.8 cm
canard area 0.35 m2
canard airfoil section NACA-4412
vertical fin NACA-0012
Length overall 288 cm
Height overall 90.88 cm
Body diameter 25 cm
propeller Diameter 61 cm
Max. launching weight 83 kg
Max. payload weight 40 kg
Launching speed 64 Knots
Cruise speed 165 Knots
Endurance 1.5 h (Can be increased)
Engine Type WAE-342
No. of cylinders 2
Engine volume 342 cc
Max. power 25 hp
Max. RPM (with propeller installed) 7000-7500
Weight 8.5 kg
Fuel type Mixture of oil and Benzene
ceiling 8000-10000 ft
Max. Thrust 65-70 lb
Fuel tank capacity 17 lit
Engine Type Vanckle Engine P73 rotary engine
Engine volume 208 cc chamber size
Max.power 30 hp
Max. RPM 8000-8500
Weight 10 kg
Fuel type Mixture of oil and Benzene
Ceiling 15000-17000 ft
Max. Thrust 75-80 lb



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