The project was initiated in August 2012 after a phone talk to Eugene Zakharenkov with a goal to build the fastest in the world unlimited aerobatics self-launching glider.
The glider features carbon fiber composite structures, symmetrical wing airfoil, jet engine H250 of Jetbeetle, 60l fuel capacity.
PRELIMINARY DATA SHEET
|Never Exceed Speed Vne, km/h (knots)||460 (250)|
|L/D Ratio (expected)||30|
|Roll Rate, deg/s||100|
|Engine Max TO Thrust, kg (lbs)||125 (275)|
|Engine Max Continuos Thrust, kg (lbs)||113 (250)|
|Limit Load Factor||+10/-10|
|Wing Span, m||11.00|
|Wing Area, sqm||9.40|
|Primary Structures Materials||Carbon Fiber Composites|