ulf 1
Technical data
Type description | ULF-1, foot-launched sailplane | ||
Type responsibility | Dieter Reich | ||
Take-off by | Foot launch (down hill), rubber cord (down hill), hang glider winch tow, car tow, air tow (trike) | ||
Wing | Cantilever structure. Shoulder mounted, single wooden spar, plywood nose section, and wooden ribs, fabric covered. | ||
Fuselage | Wooden frame of triangular cross section, fabric covered | ||
Tail | Cantilever structure, fabric covered | ||
Landing Gear | Nose skid, centre wheel, tail-skid (fibre glass tube) | ||
Accommodation | Sliding seat, open or closed cockpit | ||
Rescue system | IFuselage integrated, consisting of parachute, release unit, pull-out rocket | ||
Instruments | Air speed indicator, rate of climb indicator, altimeter | ||
Dimensions | Wing span | 10,40 m | 34.12 ft 18.21 ft |
Areas | Wing gross Vertical tail Horizontal tail | 13,4 m² | 144.18 sq.ft 16.14 sq.ft 25.82 sq.ft |
Masses | Mass empty (without rescue system) Max. take-off mass | 55 kg 155 kg | 121 lbs 342 lbs |
Ultimate Structural | Positiv | 6 g | |
Performance | Best glide ratio | 16 bei 55 km/h 0,8 m/s 33 km/h 80 km/h | 34 mph 157 fpm 21 mph 50 mph |