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Model: ST-300

The ST-300 is a UAV designed for stable and efficient operation across a wide range of altitudes and flight conditions. It operates most effectively between 400 and 2,000 meters, with a minimum allowable altitude of 60 meters, and can reach up to 5,000 meters using its internal combustion engine or 6,000 meters with its electric motor.

In terms of performance, the ST-300 delivers a maximum speed of 25 m/s, with a cruise speed of 18–20 m/s for optimal efficiency. It maintains controlled flight at lower speeds down to 18 m/s, with a stall speed ranging between 14 and 16 m/s, ensuring reliable handling and operational stability.

Aircraft Dimensions

Wingspan: 3,000 mm

Length: 1,000 mm

Height: 70 mm

Aerodynamic Efficiency (L/D ratio): 12

Flight Capabilities

Maximum Altitude:
• Internal Combustion Engine (ICE): 5,000 m
• Electric Motor: 6,000 m

Minimum Allowable Altitude: 60 m

Operational Altitude Range: 400–2,000 m

Speed & Performance

Maximum Speed: 25 m/s
Cruise Speed: 18–20 m/s
Minimum Speed: 18 m/s
Stall Speed: 14–16 m/s

Flight Time

Up to 3.5 hours

Weight & Load

Aircraft Weight: 10 kg

Maximum Takeoff Weight: 11,5 kg

Communication & Control

Max. Radio Communication Range: 100 km
Max. Video Transmission Range: 70 km

Live Photo Transmission: Available

Wind Resistance

Max. Allowable Wind Speed in Flight: 16 m/s

Max. Wind Speed for Takeoff & Landing: 8 m/s

Environmental Tolerance

Operational Humidity: Up to 98%

Temperature Range: -20°C to +50°C

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