New Elektra Two Solar Electric Aircraft For Sale
Robust design, can fly in low turbulence conditions, very low noise pattern (under 50 dB), simple logistics, no part is longer than 12m so can be transported in a 12m trailer on normal roads, operation costs about 120 EUR/hour.
| Type: Airplane (Electric Aircraft) |
|---|
| Manufacturer: Elektra Solar |
| Model: Elektra Two Solar |
| Year: New |
| Serial Number: TBA |
| Reg. Number: TBA |
| Total Time: Delivery Hours Only |
| Seats: 2 |
| Price: Price upon request |
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
Max. glide ratio – >1:40
Certification – LTF-UL-2020 (German ultralight class) / according to country-specific regulations
Seats – 1/2 / –