Electra One

Elektra One Solar is a single-seat solar-electric aircraft developed by PC-Aero. The aircraft was unveiled at AERO Global Show for General Aviation held in Friedrichshafen, Germany, in 2012.

The aircraft’s flight tests in Alps mountain region in German municipality of Unterwössen began in June 2015. The aircraft crossed the Alps crossing over the Grossglockner at an altitude of more than 3,000m and landed after approximately two hours and 190km of flight at the airfield in Zell am See in July 2015.

"Swiss company SolarXplorer placed an order to supply one prototype of Elektra One Solar aircraft."

PC-Aero is expected to obtain type certification for Elektra One Solar from Germany for ultralight class (LTF-UL) in 2016. The company also plans to obtain FAR 103 ultralight class certification for the aircraft in future. Electra Two Record and Electra Two Standard are two other variants of the aircraft that are currently under development.

Swiss company SolarXplorer placed an order to supply one prototype of Elektra One Solar aircraft.

Elektra One solar aircraft design and features

Elektra One Solar was developed based on the fuselage of the Elektra One battery-powered model. The solar-electric aircraft includes a longer wind span with 6m² solar cells on its surface offering more than 1kW power for flying. It can fly for more than three hours without CO2 emissions and without noise.

The aircraft will be produced in different versions ranging between 8.6m and 15m wing spans. Its external dimensions include wingspan of 11m, and wing surface of 8.2m². It is built with carbon composite lightweight materials, while the solar cells were produced by SolarWorld. It features autonomous flight controls, which are also made of composite materials. The aerodynamic drag is reduced because of the new upgraded wing.

The aircraft comes with a mobile electric charging station, a solar hangar and a solar trailer. It is equipped with an onboard 5cm resolution camera for 3D landscape mapping, which was developed by partner company Elektra UAS.

Electric-solar systems and performance details

The aircraft is fitted with 280 solar cells on the wing surface, which provide approximately half of the energy required for flying. It is additionally powered by an electric motor combined with modern Li-Ion batteries of 11.5kWh, which generate approximately 16kW of constant power. The aircraft uses 2.5kW power in horizontal flight.

The maximum endurance of the aircraft exceeds eight hours, while the cruise speed is 140km/h over a maximum range of 1,000km. The empty weight of the aircraft is 100kg, battery weight is 100kg, and maximum take-off weight is 300kg with a payload capacity of 100kg. The aspect ratio of the aircraft is 14:7 and best glide ratio is 30.