| Type |
Single seat experimental glider |
| Dimensions |
Length 4 m, span 8 m, wing area 11 m2 |
| Weights |
Empty 45 kg |
| Performance |
|
| Type |
Werk.Nr |
Registration |
History |
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Designed by E. Langer, built by the Hannoversche Waggonfabrik, A.-G in 1923 |
The next construction did not have a long life. From the outset called an experimental design, a wing-controlled small glider built at the HAWA, the "Spatz". The tail end of the fuselage was a pure damping surface. To control, both wing tips were designed as a pendulum tail. For aileron, elevator and rudder control both surfaces could be moved individually. The design seems to be diffcult in control.during flight
