The Stralpes Aéro ST-11 is a French single-seat club-class sailplane designed by Christian Brondel and built by Stralpes Aéro of Challes-les-Eaux.
Design and development The ST-11 is a cantilever mid-wing monoplane with a cruciform tail and the prototype first flew on 29 August 1982. The landing gear is a fixed semi-recessed monowheel gear and a tailskid, the enclosed single-seat cockpit has a one-piece canopy.
ST-11M Minimus A powered motor-glider version.
Specifications Data from Jane's All the World's Aircraft 1989-90General characteristics Crew: 1 Length: 5.55 m (18 ft 2.5 in) Wingspan: 11.60 m (38 ft 0.25 in) Height: 1.135 m (3 ft 8.75 in) Wing area: 6.54 m2 (70.4 sq ft) Aspect ratio: 20.6 Empty weight: 110 kg (243 lb) Gross weight: 230 kg (507 lb) Performance
Maximum speed: 230 km/h (143 mph, 124 kn) Stall speed: 68 km/h (42 mph, 36 kn) g limits: +5.3/-2.65 Maximum glide ratio: 35 Rate of sink: 0.65 m/s (128 ft/min)
See also
Related lists
List of gliders
References
