Starck AS.20
| AS.20 | |
|---|---|
 | |
| General information | |
| Type | Experimental aircraft |
National origin | France |
| Designer | |
| Number built | 1 |
| History | |
| First flight | 23 October 1942 |
The Starck AS.20 was an experimental single seat narrow-gap biplane built in France in the early 1940s. Despite the occupation of France, construction continued into 1941.
Specifications
Data from
General characteristics
- Crew: 1
- Length: 5.30 m (17 ft 5 in)
- Wingspan: 5.84 m (19 ft 2 in)
- Wing area: 8.00 m2 (86.1 sq ft)
- Empty weight: 226 kg (498 lb)
- Gross weight: 373 kg (822 lb)
- Powerplant: 1 × Régnier 4D2 air-cooled flat four, 55 kW (74 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 240 km/h (150 mph, 130 kn)
- Range: 1,400 km (870 mi, 760 nmi)
- Service ceiling: 7,500 m (24,600 ft)
References
- ↑ "Stark AS20 of 1942 - Rare Birds (6)". Falkeeinsgreatplanes.blogspot.com. 24 January 2010. Retrieved 10 March 2019.
- ↑ "Starck AS-20". Aviafrance.com. Retrieved 10 March 2019.
External links
Wikimedia Commons has media related to Starck AS-20.
- "Matériel Volant: Avion Starck (Type A.S. 20 Moteur Régnier 74 CV.)". L'Aérophile (in French). Vol. 51, no. 4. April 1943. pp. 66–67.