SZD-51 Junior

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
SZD-51 Junior
Polish SZD-51-1 Junior glider.jpg
Role Sailplane
National origin Poland
Manufacturer PZL Bielsko
Designer Stanislaw Zientek
First flight 31 December 1980
Number built 261
Developed from SZD-47

The PZL Bielsko SZD-51 Junior is a Polish single-seat training and club sailplane.


The Junior was designed by Stanislaw Zientek, based on the SZD-47 which had originally been developed in the years 1973 - 1974 at the Research and Development Center in Bielsko-Biała. The prototype SZD-51-0 was first flown on 31 December 1980, and was followed by the production version, the SZD-51-1, with a modified fuselage, A total of 261 aircraft were built. The type was proposed for licence production in Brazil, but in the event only a single SZD-51-1 was built there. The simplified SZD-51-2 was a runner up in the IGC World Class design contest.


The SZD-51-1 "Junior" is a single-seat glider of fiberglass construction. Only the rudder is fabric covered. The fuselage has an internal tubular steel frame. The aircraft has a two-piece wing with a spar, and a fixed main wheel. The Schempp-Hirth type airbrakes are fitted only on the top surface of the wing. Rudder pedals are adjustable. The control for the rudder via cables, all other control surfaces are operated by rods. The Junior is characterized by good slow flight characteristics and is very forgiving in flight behaviour. The aircraft is designed for early solo and club flying, but is certified for aerobatics and can be equipped for high-altitude flight and cloud flying.

Specifications (SZD-51-1)[edit]

Data from Jane's All the World's Aircraft 1988-89[1]

General characteristics

  • Crew: 1
  • Length: 6.69 m (21 ft 11 in)
  • Wingspan: 15 m (49 ft 3 in)
  • Height: 1.54 m (5 ft 1 in)
  • Wing area: 12.51 m2 (134.7 sq ft)
  • Aspect ratio: 18
  • Airfoil: root:Wortmann FX-S-02-196; tip:FX-S-02/1-158
  • Empty weight: 242 kg (534 lb)
  • Max takeoff weight: 355 kg (783 lb)


  • Stall speed: 60 km/h (37 mph, 32 kn)
  • Never exceed speed: 220 km/h (140 mph, 120 kn) in smooth air
  • Max rough air speed: 150 km/h (81 kn; 93 mph)
  • Max aero-tow speed: 140 km/h (76 kn; 87 mph)
  • Max winch-launch speed: 128 km/h (69 kn; 80 mph)
  • Maximum glide ratio: 35
  • Best glide speed: 80 km/h (43 kn; 50 mph)
  • Rate of sink: 0.59 m/s (116 ft/min) at 72 km/h (39 kn; 45 mph)
  • Wing loading: 28.4 kg/m2 (5.8 lb/sq ft)

See also[edit]

Aircraft of comparable role, configuration and era Schleicher ASK 23 Related lists List of gliders


  1. ^ John W.R. Taylor, ed. (1988). Jane's All the World's Aircraft 1988-89. London: Jane's Information Group. p. 638. ISBN 0-7106-0867-5.

External links[edit]

Media related to SZD-51-1 Junior at Wikimedia Commons