Vladimir Talanczuk
| Wladimir Talanczuk | |
|---|---|
| Born | Ukraine, USSR |
| Nationality | Ukrainian - Canadian |
| Education | Institute for Aviation Specialists, Poland |
| Occupation | Engineer |
| Engineering career | |
| Institutions |
AeroKlub Wrocław Birdman Enterprises |
| Projects | Birdman WT-11 Chinook |
| Significant advance |
Ultralight aircraft Hang gliders |
Wladimir Talanczuk (also known by his anglicized name Vladimir Talanczuk) is a Ukrainian- born aeronautical engineer known for his hang glider and ultralight aircraft designs.
Talanczuk graduated from the Polish Institute for Aviation Specialists in 1970 as an aeronautical engineer and immediately embarked upon a career as a designer of hang gliders and light aircraft. He worked with Tadensca Dobczynski, the Polish amateur aircraft builder, assisting in the design and construction of more than thirty Dobczynski designs.
Talanczuk qualified as a light aircraft pilot, logging 1200 hours of flight time. In 1972 he began to seriously devote his time to hang gliding. While working for the AeroKlub Wrocław he designed his Mars series of hang gliders, including the WT-6 Mars-S, WT-7 Mars-2S and WT-8 Mars-Agat. Throughout 1979 he was a member of the Polish National Hang Gliding Team and competed in the World Hang Gliding Championships at Grenoble, France, flying a Mars hang glider of his own design. The hang glider he flew at that event was at that time the largest wingspan hang glider flown.
Talanczuk also served as a consultant to the Polish National Aero Club in the fields of accident investigation and analysis. He designed several light aircraft and completed a single-seat gyroplane during his time in Poland.
He emigrated to Canada in 1981 and began working for hang glider and ultralight aircraft manufacturer Birdman Enterprises, of Edmonton, Alberta shortly after his arrival, filling the position of Chief Engineer and Designer.
Talanczuk's first project at Birdman was the design of a new ultralight aircraft to replace the Birdman Atlas in production. The company's stated design goals for the aircraft were: good flying characteristics, simplicity of construction and maximization of aesthetics.
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