Engineering:SFAN II
From HandWiki
Revision as of 08:43, 1 June 2021 by imported>CodeMe (update)
Short description: 1930s French aircraft
| SFAN II | |
|---|---|
| Role | Ultralight aircraft |
| National origin | France |
| Manufacturer | SFAN |
| First flight | 1935 |
The SFAN II was a French motorglider built in the mid-1930s.
Specifications
Data from J2mcL Planeurs,[1] Aviafrance : S.F.A.N. II[2]
General characteristics
- Crew: 1
- Length: 6.72 m (22 ft 1 in)
- Wingspan: 12 m (39 ft 4 in)
- Height: 2.27 m (7 ft 5 in)
- Wing area: 16.5 m2 (178 sq ft)
- Empty weight: 200 kg (441 lb)
- Max takeoff weight: 315 kg (694 lb)
- Powerplant: 1 × Ava 4A-00 4-cylinder air-cooled horizontally-opposed piston engine, 19 kW (25 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 115 km/h (71 mph, 62 kn)
- Wing loading: 19.1 kg/m2 (3.9 lb/sq ft)
See also
Related development
References
- ↑ "J2mcL Planeurs - Fiche planeur n°2209" (in Fr). https://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/planeur-fiche_0int.php?code=2209. Retrieved 26 February 2019.
- ↑ "S.F.A.N. II - Motoplaneur - Un siècle d'aviation française" (in fr). Aviafrance.com. 2005-12-10. https://www.aviafrance.com/s-f-a-n-ii-aviation-france-10005.htm. Retrieved 2019-02-26.
 |  |
