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.

AS.20
Role	Experimental aircraft Type of aircraft
National origin	France
Designer	André Starck
First flight	23 October 1942
Number built	1

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

Wikimedia Commons has media related to Starck AS-20.

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.