Sparmann S-1
Sparmann S-1 | |
---|---|
Role | Training monoplane |
National origin | Sweden |
Manufacturer | Sparmann |
Primary user | Swedish Air Force |
|
The Sparmann S-1 was a 1930s Swedish military training monoplane, designed by Edmund Sparmann, built in small numbers for the Swedish Air Force. The S-1 was a single-seat low-wing braced-monoplane with a fixed trail-skid landing gear. It was powered by a single 130 hp (97 kW) de Havilland Gipsy Major engine.
Operators
Specifications
Data from [1]
General characteristics
- Length: 6.18 m (20 ft 3 in)
- Wingspan: 8 m (26 ft 3 in)
- Max takeoff weight: 625 kg (1,378 lb)
- Powerplant: 1 × de Havilland Gipsy Major 4-cyl. invewrted air-cooled in-line piston engine, 97 kW (130 hp)
Performance
- Maximum speed: 250 km/h (155 mph; 135 kn)
See also
- Related lists
Notes
- ↑ Henriksson, Lars. "P 1 - Sparmann S 1-A "Sparmannjagaren" (1939-1947)". Retrieved 10 June 2013.
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
- Henriksson, Lars. "P 1 - Sparmann S 1-A "Sparmannjagaren" (1939-1947)". Retrieved 10 June 2013.
This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.