Sparmann S-1
From Infogalactic: the planetary knowledge core
(Redirected from Sparmann S-1A)
| 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
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
References
- Lua error in package.lua at line 80: module 'strict' not found.
- Lua error in package.lua at line 80: module 'strict' not found.
- Lua error in package.lua at line 80: module 'strict' not found.
