Swiss SGS 1-34
| Swiss SGS 1-34 | |
|---|---|
 SGS 1-34 |
|
| Type: | Glider |
| Design country: | |
| Manufacturer: | |
| First flight: |
1969 |
| Number of pieces: |
98 |
The Swiss SGS 1-34 is an American standard class glider in all-metal construction. 98 of the aircraft designed as a performance aircraft were produced.
construction
The SGS 1-34 is a cantilevered shoulder -wing aircraft with single-spar, metal-clad all-metal wings. Air brakes are installed above and below the wings to limit the speed . The fuselage is an all-metal shell construction. The unicycle undercarriage was available rigid or retractable.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| length | 7.8 m |
| span | 15 m |
| height | |
| Wing area | 14 m² |
| Wing extension | 16.1 |
| Wing loading | |
| Wing profile | |
| Glide ratio | 33 at 88 km / h |
| Slightest sinking | |
| Empty mass | 259 kg |
| Max. Takeoff mass | 381 kg |
| Top speed | 227 km / h |
See also
Web links
Commons : Schweizer SGS 1-34 - Collection of images, videos and audio files
