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R-UAV-011
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The fuselage of the Six-Rotor R-UAV-011 is made of high-strength and high-rigidity carbon fibre composite material, one-time molded.The UAV can carry loads of different weights and adapt to high-altitude operations. It can carry small caliber mortar shells and complete shell dropping via ground station. The UAV supports the mounting of a high-performance electro-optical pod, high-speed data link equipment and warhead, and is equipped with a dedicated ground station system. R-UAV-011 has a payload of 4 to 6kg, a maximum take-off weight of 18kg, a maximum flight speed of 72km/h, and an endurance of 50 minutes.
Technical Specifications
Fuselage Height | 560±20mm |
Distance Between Symmetrical Motor Shafts | 1290mm |
Fuselage Materials | Imported carbon fibre, fireproof, rainproof and dustproof |
Model | Six-axis X-shaped layout |
Maximum Take-Off Weight | ≤18kg |
Self-Weight | ≤3.5kg (Battery excluded) |
Payload | 4kg~6kg |
Power Battery Voltage | 12S Lithium |
Endurance | 50min (No load) 30min (Full load) (Up to 1000m above sea level, 25°C) |
Blade | 22~24 inches (Change according to the environment) |
Maximum Flight Speed | 72km/h |
Maximum Climbing Speed | 18km/h |
Maximum Descending Speed | 7.2km/h |
Relative Flight Altitude | 3000m (Plain) |
Maximum Operating Altitude | 5000m (Relative height 2000m) |
Wind Resistance Capability | Level 6 (10.8m/s-13.8m/s) |
Operating Temperature | -20℃~55℃ |
GPS Hovering Accuracy | Horizontal: ±2m; Vertical: ±1.5m |
Remote Control Distance | 10km (Depends on the local electromagnetic environment) |
Graphical Transmission Distance | 20km (Thorough vision) |
Ground Station Control Distance | 20km (Thorough vision) |
Motor | T-motor 6015/6215/X6 |
Electronic Speed Control | T-motor 60A |
| Flight Cases | A big one and a small one |
The fuselage of the Six-Rotor R-UAV-011 is made of high-strength and high-rigidity carbon fibre composite material, one-time molded.The UAV can carry loads of different weights and adapt to high-altitude operations. It can carry small caliber mortar shells and complete shell dropping via ground station. The UAV supports the mounting of a high-performance electro-optical pod, high-speed data link equipment and warhead, and is equipped with a dedicated ground station system. R-UAV-011 has a payload of 4 to 6kg, a maximum take-off weight of 18kg, a maximum flight speed of 72km/h, and an endurance of 50 minutes.
Technical Specifications
Fuselage Height | 560±20mm |
Distance Between Symmetrical Motor Shafts | 1290mm |
Fuselage Materials | Imported carbon fibre, fireproof, rainproof and dustproof |
Model | Six-axis X-shaped layout |
Maximum Take-Off Weight | ≤18kg |
Self-Weight | ≤3.5kg (Battery excluded) |
Payload | 4kg~6kg |
Power Battery Voltage | 12S Lithium |
Endurance | 50min (No load) 30min (Full load) (Up to 1000m above sea level, 25°C) |
Blade | 22~24 inches (Change according to the environment) |
Maximum Flight Speed | 72km/h |
Maximum Climbing Speed | 18km/h |
Maximum Descending Speed | 7.2km/h |
Relative Flight Altitude | 3000m (Plain) |
Maximum Operating Altitude | 5000m (Relative height 2000m) |
Wind Resistance Capability | Level 6 (10.8m/s-13.8m/s) |
Operating Temperature | -20℃~55℃ |
GPS Hovering Accuracy | Horizontal: ±2m; Vertical: ±1.5m |
Remote Control Distance | 10km (Depends on the local electromagnetic environment) |
Graphical Transmission Distance | 20km (Thorough vision) |
Ground Station Control Distance | 20km (Thorough vision) |
Motor | T-motor 6015/6215/X6 |
Electronic Speed Control | T-motor 60A |
| Flight Cases | A big one and a small one |
