Elektra one Solar

Single-seat Solar-powered Aircraft

Elektra One Solar is A single-seat aircraft system with Solar cells (no autopilot)

Application

The design and manufacture of the aircraft is state-of-the-art, consisting of the best possible aerodynamic flight characteristics and the highest level of safety. The Elektra One is made of the best materials (state-of-the-art carbon fiber technology) and the efficiency of its propeller is 90%.

Depending on wind conditions, a flight duration of at least 3 hours and a range of 400km can be achieved with the aid of the redundant, highly efficient electric drive. With a low noise level of less than 50dB and a propeller speed of 1,400 revolutions per minute (RPM), the aircraft glides through the air almost silently. The aircraft is approved in the German LTF UL class.

Description

The design and manufacture of the aircraft is state-of-the-art, with the objectives of the best possible aerodynamic flight characteristics, the highest safety and the selection of the best materials. The structure of Elektra One Solar consists of state-of-the-art carbon fiber technology. The efficiency of the propeller is 90%.

Depending on the wind conditions, a flight duration of at least 3 hours and a range of 400 km can be achieved with the aid of the redundant, highly efficient electric drive. With the low noise level of less than 50dB and a propeller speed of 1400 rounds per minute, the aircraft glides through the air almost silently. The aircraft is approved in the German LTF UL class.

Elektra One Solar is also available as a Optional Piloted System (OPS) and Unmanned Aircraft System (UAS).

Technical specs

Elektra one Solar

SPECS
ELEKTRA ONE SOLAR
Seats
1
Electric Motor
32 kW (continous power), double redundant system
Propeller speed for cruise
1.400 rpm
Wing span
13 m
Wing surface
10 m²
Maximum weight
300 kg
Tare w/o battery
120 kg
Battery weight
60 kg
Maximum payload
100 kg
Maximum flight duration*
5 hours
Range
>400 km
Cruising speed

Power needed for horizontal flight

Max. power provided by solar cells
100 km/h

3.5 kW

1.5 kW
Wing aspect ration
16.9
Max. glide ratio
> 1:30
Certification
LFT-UL Deutschland
*Depending on wind conditions

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