Starck AS.20

AS.20
AS.20
General information
Type	Experimental aircraft
National origin	France
Designer	André Starck
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

"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.

[1] "Stark AS20 of 1942 - Rare Birds (6)". Falkeeinsgreatplanes.blogspot.com. 24 January 2010. Retrieved 10 March 2019.

[2] "Starck AS-20". Aviafrance.com. Retrieved 10 March 2019.