In the last 10 years there have been significant developments in hang glider wings. That may come as a surprise to KITPLANES® readers. After all, the wings don’t look much different from one another, so the changes must be subtle, right? Well, yes and no. In fact, many subtle changes have occurred as these wings have steadily progressed from a glide angle of 4:1 in the 1970s to the 15:1 glides that are common today. Even as they gained efficiency, the wings haven’t changed a lot in appearance. But not all of the changes are so subtle. The ATOS VX I flew in late 2004 illustrates a radically different approach to wing design. The ATOS VX can achieve a glide angle of 20:1 and a sink rate of only 118 fpm. The latter number makes this wing competitive with many sailplanes, even though the pilot hangs in the airstream. An Innovative Design The design is produced by Aeronautic Innovation Rühle (AIR) and is the creation of Felix Rühle, who worked with composite materials for many years in his role with the German government’s Center for Research and Development in Aerospace Technology in Stuttgart.
State of the Art in Hang Gliding
It's a tight fit in that control bar, but two people did not seem to affect the ATOS VX's performance. The "student" (the author, right) holds onto the harness of the instructor (designer Felix Rühle) so as not to interfere during the critical launch phase. (Rühle put on his helmet after the photo was taken.)
Just off the ground on aero tow via ultralight, this ATOS heads aloft for certain soaring flight. A 20:1 glide and 118-fpm sink rate help any pilot.
This early ATOS is about to undergo torturous load testing atop the German DHV test rig. The high mount assures the wing cuts through clean air.
The beautifully slender high-aspect-ratio wing is a graceful sight. The dark areas at the wingroot are the carbon-fiber flaps that can be lowered for launch, landing and thermal flying.
The ATOS VX is a fully cantilevered wing. This view under the nosecone shows the many custom-designed components that hold the wing halves at the proper angle.