page_title: Orlican VSO 10
section_title: Specifications (VSO 10)
hierarchical_section_title: Orlican VSO 10 / Specifications (VSO 10)
caption_attribution_description: Vosa VSO-10 Aeroklubu Praha Let%u0148any - airfield Havlí%u010Dk%u016Fv Brod
context_page_description: The VSO 10 Vosa is a Standard and Club-Class glider designed and manufactured in the Czechoslovak Republic from December 1978 as a replacement for the VT-116 Orlik II.
context_section_description: Data from Jane's All the World's Aircraft 1988-89
  General characteristics
  Crew: one
  Length: 7 m (23 ft 0 in)
  Wingspan: 15 m (49 ft 3 in)
  Height: 1.38 m (4 ft 6 in)
  Wing area: 12 m² (130 sq ft)
  Airfoil: root:Wortmann FX-61-163 ; tip:Wortmann FX-60-126
  Empty weight: 250 kg (551 lb)
  Max takeoff weight: 380 kg (838 lb)
  Performance
  Stall speed: 68 km/h (42 mph, 37 kn)
  Never exceed speed: 250 km/h (160 mph, 130 kn) in smooth air
  160 km/h (86 kn; 99 mph) in rough air
  160 km/h (86 kn; 99 mph) on aero-tow
  120 km/h (65 kn; 75 mph) on winch launch
  g limits: +5.3 -3.5
  Maximum glide ratio: 36 at 90 km/h (49 kn; 56 mph)
  Rate of sink: 0.64 m/s (126 ft/min) at 73 km/h (39 kn; 45 mph)
  Wing loading: 31.67 kg/m² (6.49 lb/sq ft) max
caption: Image of VSO-10B showing the fixed forward segment of its canopy, and the removable rear segment that allows access by the pilot
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