Elektra SolarSingle-engine piston · Bavaria, Germany, Landsberg am Lech
2023 New Elektra Two Solar Electric
- Price
- On request
- Year
- 2023
- Total time
- 1 hours
- Location
- Germany
Specifications
General
- Registration
- TBA
- Total time
- 1
- Seats
- 2
- Condition
- New
- Type
- Electric Powered Aircraft
- Sale
- aircraft for sale
Description
- Max. glide ratio – >1
- 40
Description
OPS version
- Elektra Two Solar OPS can be operated conventionally by a regular pilot or an autopilot for the entire flight from takeoff to landing. The pilot can switch to the autopilot mode & can fly a mission completely autonomously including take-off & landing. The flight mission can be defined by means of a special software before the flight & changed or adapted during the flight from the cockpit or from the ground control station. The solar system extends the flight endurance & range.
- UAS version
- The Elektra Two Solar UAS (unmanned) is based on the OPS version. Removing some parts like the instrument panel, flight controls, canopy, seat & safety belts reduces the aircraft weight by 20 kg allowing for increasing the payload or battery capacity. The UAS version is designed to fly up to 20 km altitude.
- Redundancy
- Dual redundant propulsion system. Each of two subsystems is composed of motor, motor controller, battery. Dual redundant power supply for avionics & autopilot. In case of failure of motor, motor controller, battery or all of them in one subsystem, the aircraft is able to climb with at least 1.5 m/s. In case of OPS, double redundant electronic flight instruments.
- Performance (OPS / UAS)
- Cruise speed (IAS) – 75 km/h
- Stall speed VS – 55 km/h
- VNE (IAS) – 150 km/h
- Max. vertical climb speed – 3 m/s
- Take-off distance – 100 m
- Landing distance – 200 m
- Max. flight duration – > 12 hours / > 18 hours
- Powerplant (OPS / UAS)
- Max. peak power – 32 kW
- Max. continuous power (MCP) – 20 kW
- Cruise power – 5 kW
- Solar surface – >23,5 m² / 25 m²
- Max. solar power – >5 kW (low altitude) / >5 kW (low altitude)²
- Weights (OPS / UAS)
- Max. take-off weight (MTOW) – 600 kg
- Max. battery weight – 200 kg / 300 kg
- Max. payload weight – 100 kg
- Max. pilot weight – 110 kg / –
- Empty weight (w/o battery) – 270 kg / 250 kg
- Other Data (OPS / UAS)
- Wingspan – 27 m
- Wing surface – 28.6 m²
- Wing aspect ratio – 23
- Electric variable pith propeller
- Emergency parachute included
- Certification – LTF-UL-2020 (German ultralight class) / according to country-specific regulations
- Seats – 1/2 / –