| Swift S-1 | |
|---|---|
![]()  | |
| Role | Aerobatic glider | 
| Manufacturer | Swift Ltd. | 
| Designer | Edward Marganski and Jerzy Cisowski | 
| First flight | 6 August 1991 (proof of concept glider: 11 January 1991) | 
| Primary users | Jerzy Makula see European and World Glider Aerobatic Championships for further users  | 
| Produced | 1991–1997 | 
| Number built | 30 (+ proof of concept glider) | 
| Developed from | SZD-21 Kobuz | 
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.[1][2] 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 [1]
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
References
Wikimedia Commons has media related to Swift S-1.
- 1 2 ""SWIFT" S-1". marganski.com. Retrieved 30 January 2019.
 - ↑ "Swift S-1". www.sagach.ch (in German). Retrieved 30 January 2019.
 
External links
    This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.


