The Swift S-1 is a single seat aerobatic glider manufactured by Polish company Swift Ltd.
Design and development Edward Margański, Jerzy Cisowski and Jerzy Makula developed the Swift at Bielsko-Biała from the SZD-21-2b Kobuz 3. The prototype first flew in 1991. The glider is made of glass-fibre epoxy composite. It is very strong (stressed for plus and minus 10g) and manoeuvrable (a roll takes less than 4 seconds). Larger tips to increase the span to 15m were designed but not made. It has a retractable undercarriage.
Specifications Data from General characteristics Crew: 1 Length: 6.91 m (22 ft 8 in) Wingspan: 12.7 m (41 ft 8 in) Wing area: 11.8 m2 (127 sq ft) Tailplane area: 1.65 m2 (17.8 sq ft) Fin area: 0.9 m2 (9.7 sq ft) Aspect ratio: 14.3 Airfoil: NACA 641412 Tailplane airfoil: NACA 631012-63006 Fin airfoil: NACA 632015-63012 Empty weight: 280 kg (617 lb) Gross weight: 390 kg (860 lb) Performance
Never exceed speed: 320 km/h (200 mph, 170 kn) diving Maximum manoeuvring speed: 228 km/h (142 mph; 123 kn) g limits: +10 g / - 7.5 g Maximum glide ratio: 30:1 at 107 km/h (66 mph; 58 kn) Rate of sink: 0.9 m/s (180 ft/min)
Gallery
Comparable aircraft Celair GA-1 Celstar MDM-1 Fox PZL Bielsko SZD-59
References
External links GoPro Hero 2 Swift S-1 2012 by Luca Bertossio in 3D




