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 |
