Engineering:Starck AS.20
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Revision as of 14:39, 30 May 2022 by imported>StanislovAI (fix)
| AS.20 | |
|---|---|
| |
| Role | Experimental aircraft |
| National origin | France |
| Designer | André Starck |
| First flight | 23 October 1942 |
| Number built | 1 |
The Starck AS.20 was an experimental single seat biplane built in France in the early 1940s.[1] Despite the occupation of France, construction continued into 1941.
Specifications
Data from [2]
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)". 24 January 2010. https://falkeeinsgreatplanes.blogspot.com/2010/01/stark-as20-of-1942.html. Retrieved 10 March 2019.
- ↑ "Starck AS-20". https://www.aviafrance.com/starck-as-20-aviation-france-647.htm. Retrieved 10 March 2019.
External links
- "Matériel Volant: Avion Starck (Type A.S. 20 Moteur Régnier 74 CV.)" (in French). L'Aérophile 51 (4): 66–67. April 1943. https://gallica.bnf.fr/ark:/12148/bpt6k6567839v/f10.image.
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