:Starck AS.20
| {{Infobox Aircraft Begin
| name=AS.20 | image= Starck AS-20 right photo L'Aerophile April 1943.jpg | caption= }}{{Infobox Aircraft Type | type=Experimental aircraft | national origin=France | manufacturer= | designer=André Starck | first flight=23 October 1942 | introduced= | retired= | status= | primary user= | more users= | produced= | number built=1 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Starck AS.20 was an experimental single seat biplane built in France in the early 1940s.{{cite web |title=Stark AS20 of 1942 - Rare Birds (6) |url=https://falkeeinsgreatplanes.blogspot.com/2010/01/stark-as20-of-1942.html |website=Falkeeinsgreatplanes.blogspot.com|accessdate=10 March 2019 |date=24 January 2010}} Despite the occupation of France, construction continued into 1941.
Specifications
{{Aircraft specs
|prime units?=met
|genhide=
|crew=1
|capacity=
|length m=5.30
|span m=5.84
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=8.00
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=226
|empty weight lb=
|empty weight note=
|gross weight kg=373
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Régnier 4D2
|eng1 type=air-cooled flat four
|eng1 hp=74
|eng1 note=
|power original=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|perfhide=
|max speed kmh=240
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=1400
|range note=
|endurance=
|ceiling m=7500
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|more performance=
}}
References
{{Reflist}}
External links
{{commons category}}
- {{cite magazine |title=Matériel Volant: Avion Starck (Type A.S. 20 Moteur Régnier 74 CV.) |magazine=L'Aérophile |date=April 1943 |volume=51 |issue=4 |pages=66–67 |language=French |url=https://gallica.bnf.fr/ark:/12148/bpt6k6567839v/f10.image |ref={{harvid |L'Aérophile April 1943}} }}
{{Starck aircraft}}
Category:1940s French aircraft