SDO 50 V2 Helicopter UAV
Product descripton: SDO 50 V2 Helicopter UAV by SwissDrones
The SDO 50 is engineered to operate in difficult or dangerous environments where manned aircraft cannot safely perform. Its vertical take-off and landing capability, high-end sensor integration, and robust autonomous flight systems make it ideal for missions in challenging weather, darkness, or hostile areas.
Key Advantages
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Risk Reduction: Safely perform missions in extreme conditions or unsafe areas.
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Cost Efficiency: Reduces operational expenses by up to 70% compared to manned aircraft and requires minimal training.
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CO2 Emissions Reduction: Achieves up to 95% lower emissions versus helicopters.
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Rapid Deployment: Transportable by van; a two-person crew can prepare it for flight in 15 minutes.
Payload & Sensor Capabilities
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Supports a useful payload of up to 33.2 kg (including fuel).
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Flexible integration of multiple sensors and camera systems simultaneously.
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Compatible with high-end navigation and environmental sensors for professional missions.
Flight & Operational Features
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Fully autonomous flight with high-end autopilot.
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BVLOS-capable for long-range missions (up to 216 km with communication coverage).
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Redundant systems for operational safety.
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Small operational footprint, suitable for permanent installations, ship-based operations, or ground transport.
Environmental & Performance Adaptability
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Max wind tolerance: 21.6 KTAS (40 km/h).
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Operating temperature range: –20 °C to +50 °C (–4 °F to 122 °F).
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Max operating altitude: 10,000 ft AMSL (3,048 m).
Use Cases
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Industrial inspection and monitoring
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Environmental research and data collection
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Disaster response and emergency operations
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Military and governmental missions requiring BVLOS operations
Technical specifications
| Specification | Value |
|---|---|
| Dimensions (L x W x H) | 2.32 x 0.7 x 0.92 m (7.6 x 2.3 x 3.0 ft) |
| Rotor Diameter | 2 x 2.82 m (9.25 ft) Flettner double rotor |
| Maximum Takeoff Weight (MTOW) | 87 kg |
| Dry Operating Mass | 53.8 kg |
| Useful Load | Up to 33.2 kg (including fuel) |
| Cruise Speed | 39 KTAS (72 km/h) |
| Max Endurance | 3h 02min (full fuel, no payload) |
| Engine | Single-shaft turbine |
| Fuel Type | JET A1 |
| Fuel Tank Capacity | Main: 13 L; Add-on tanks: up to 2 x 17 L |
| Fuel Consumption | 12.5 L/hour (ISA conditions) |
| Landing Gear | 3 heights |
| Set Up Time | 15 minutes |
| Autorotation | Available |
| Maximum Operating Altitude | 10,000 ft AMSL (3,048 m) |
| Max Wind Speed | 21.6 KTAS (40 km/h) |
| Operating Temperature | –20 °C to +50 °C (–4 °F to 122 °F) |
| Max Range | 216 km (subject to communication coverage) |
| Data Link Options | UHF, encrypted Mesh IP (S-Band, L-Band), 4G/LTE, SatCom |
| Traffic Avoidance | ADS-B / Mode S transponder available |
| Pilot Camera | Forward and downward views available |
| Autonomous Flight | Fully autonomous |
| Payload Electrical Power | 200 W @ 24 V DC (optional 400 W @ 24 V DC) |