- Swift S-1
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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 usersProduced 1991- 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.
Contents
Design and development
Edward Margański 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 4 seconds). Larger tips are available to increase the span to 15m. It has a retractable undercarriage.
Specifications
Data from[citation needed]
General characteristics
- Crew: 1
- Length: 6.91 m (22 ft 8 in)
- Wingspan: 12.7 (41 ft 8 in)
- Height: ()
- Wing area: 11.8 m2 (127 sq.ft.)
- Airfoil: NACA 641412
- Aspect ratio: 14.3
- Empty weight: 280 kg (617 lb)
- Loaded weight: 390 kg (860 lb)
Performance
- Maximum speed: 287 km/h (178 mph)
- sink rate: 0.9 m/s (177 ft/s)
- glide ratio: 30.0 (at 127 km/h)
- Tail area: 1.65 m²
- Tail airfoil: NACA 631012-63006
- Vertical Empennage Area: 0.9 m²
- Vertical Empennage Airfoil: NACA 632015-63012
- Manoeuver Speed Va: 228 km/h
- Diving Speed Vd: 320 km/h
- Max Lift/Drag Ratio: 30.0 @ 107 km/h
- Minimum Speed: 73 km/h
- Load Factors: +10 g / - 7.5 g
See also
Comparable aircraft
- Celair GA-1 Celstar
- MDM-1 Fox
- PZL Bielsko SZD-59
References
- ^ Margański & Mysłowski: Swift S-1 - accessed 2008-03-20
- ^ Swiss Aerobatic Gliding Association: Swift S-1 (in German) - accessed 2008-03-20
External links
Categories:- Glider aircraft
- Polish sailplanes 1990–1999
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