First ultralight helicopter with German Type Certificate
The coaxial rotor variant with four rotor blades on two rotor levels rotating in opposite
directions creates a more stable flight behavior due to its inherent stability compared to the
The entire power of the engine is used for the lift because there is no loss due to an
additional tail rotor to be driven.
We also use aerospace-approved materials in the UL area and thus guarantee a higher reliability of materials and technology.
With the revision of the original prototype, a new concept has been created in practically all
essential points, which is also reflected in the change in our type designation.
The frame, the landing gear, the rotor mast, the cabin and the tail boom represent a
milestone in the development, and, with their associated simplified production and
improved properties, they form the basis for our quality standards.
Der Rahmen, das Landegestell, der Rotormast, die Kabine und der Heckausleger stellen einen Meilenstein in der Entwicklung dar und bilden mit ihrer damit verbundenen vereinfachten Fertigung sowie den verbesserten Eigenschaften die Basis für unseren Qualitätsanspruch.
|Rotor diameter:||6,5 m|
|Empty weight:||283 kg|
Max. take-off weight:
|ca. 170 kph|
Max cruising speed:
|ca. 150 kph|
|D‑Motor (125 hp)|