![]() Dual redundant power supply for avionics and autopilot. Each of two subsystems is composed of motor, motor controller, battery. Redundancyĭual redundant propulsion system. The UAS version is designed to fly up to 20 km altitude. Removing some parts like the instrument panel, flight controls, canopy, seat and safety belts reduces the aircraft weight by 20 kg allowing for increasing the payload or battery capacity. The Elektra Two Solar UAS (unmanned) is based on the OPS version. The flight mission can be defined by means of a special software before the flight and changed or adapted during the flight from the cockpit or from the ground control station.The solar system extends the flight endurance and range. The pilot can switch to the autopilot mode and can fly a mission completely autonomously including take-off and landing. operation costs about 120 EUR/hour OPS versionĮlektra Two Solar OPS can be operated conventionally by a regular pilot or an autopilot for the entire flight from takeoff to landing. Can be transported in a 12m trailer on normal roads ![]() ![]() simple logistics: no part is longer than 12m. robust design: can fly in low turbulence conditions According to country-specific regulations ![]()
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