S-30 Conventional Layout Fixed Wing Unmanned Target System
â–² The aircraft is a conventional layout, composite fixed wing drone. The flat convex airfoil with a large lift to drag ratio exhibits excellent flight performance in both high-speed and low-speed flight, making it suitable for use as a low-speed target aircraft.
â–² The large cabin design of the fuselage facilitates the installation of various load equipment.
â–² The power is an oil powered internal combustion engine, with sufficient power, stable and reliable operation, and convenient use.
â–² The body material is a fiberglass structure with PVC interlayer. You can also choose carbon fiber or Kevlar materials for customized use according to your requirements;
â–² The aircraft can increase its fuel tank capacity to provide longer endurance, with a maximum time of up to 3 hours.
â–² The increased wing area greatly reduces the wing load, resulting in a maximum mission load of 7 kilograms.
â–² The fuselage carries a retrieval umbrella, which can be opened and landed in emergency situations, ensuring the safety of the aircraft and ground facilities.
| Name | Parameter | Name | Parameter |
| Wingspan | 3.4m | Full height | 0.7m |
| Length | 2.55m | Maximum takeoff weight | 35kg |
| Maximum Mission Load | 7kg | Takeoff and landing mode | Glide takeoff and landing or parachute landing |
| Takeoff speed | 58km/h | Landing speed | 65km/h |
| Max climb rate | 4m/s | Cruise speed | 100-110km/h |
| Maximum level flight speed | 125km/h | Maximum battery life | 3h |
| Maximum flight altitude | 5500m | Maximum wind resistance | Level 6 |
| Navigation mode | GLONASS, BDS | Dynamic system | Two stroke gasoline engine |
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