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SDO 50 V2 Helicopter UAV

Highly versatile VTOL drone designed for long-range, fully autonomous BVLOS missions with heavy payloads and minimal operational footprint.

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

  • Risk Reduction: Safely perform missions in extreme conditions or unsafe areas.

  • Cost Efficiency: Reduces operational expenses by up to 70% compared to manned aircraft and requires minimal training.

  • CO2 Emissions Reduction: Achieves up to 95% lower emissions versus helicopters.

  • Rapid Deployment: Transportable by van; a two-person crew can prepare it for flight in 15 minutes.

Payload & Sensor Capabilities

  • Supports a useful payload of up to 33.2 kg (including fuel).

  • Flexible integration of multiple sensors and camera systems simultaneously.

  • Compatible with high-end navigation and environmental sensors for professional missions.

Flight & Operational Features

  • Fully autonomous flight with high-end autopilot.

  • BVLOS-capable for long-range missions (up to 216 km with communication coverage).

  • Redundant systems for operational safety.

  • Small operational footprint, suitable for permanent installations, ship-based operations, or ground transport.

Environmental & Performance Adaptability

  • Max wind tolerance: 21.6 KTAS (40 km/h).

  • Operating temperature range: –20 °C to +50 °C (–4 °F to 122 °F).

  • Max operating altitude: 10,000 ft AMSL (3,048 m).

Use Cases

  • Industrial inspection and monitoring

  • Environmental research and data collection

  • Disaster response and emergency operations

  • 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)

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