“Comte AC-1”的意思、由来-开放百科全书

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Comte AC-1

释义

Design and development
Operational history
Operators
Specifications (AC-1)
References

name = AC-1

image = Alfred Comte AC-1.jpg

caption =

}}{{Infobox Aircraft Type

type = single-seat fighter

manufacturer = Comte

designer =

first flight = 2 April 1927

introduced =

retired =

status =

primary user = Swiss Fliegertruppe

more users =

produced =

number built = 1

unit cost =

developed from =

variants with their own articles =
}}

The Comte AC-1 was a 1920s Swiss single-seat monoplane fighter aircraft produced by Flugzeugbau A. Comte.

Design and development

The Swiss company Flugzeugbau A. Comte was established in the early 1920s to build German aircraft designs under licence. The company's first original design was the Comte AC-1, developed to meet a Swiss Fliegertruppe (Swiss Air Force) requirement for a single-seat fighter.

The AC-1 was a high-wing monoplane with fixed tailskid undercarriage. It was constructed of metal with fabric-covered wing and tail surfaces. The powerplant was a Gnome et Rhône radial engine driving a fixed-pitched two-blade propeller.

The AC-1 prototype first flew on 1927. Testing and evaluation did not result in any orders but the prototype was bought by the Swiss Fliegertrupppe. The prototype was the only unit constructed of this type.

Operational history

The prototype was acquired by the Swiss Fliegetruppe and later had the wing replaced with a wing from a Dewoitine D.9. With the new wing the aircraft was used to establish a Swiss altitude record on 19 November 1928.

Operators

{{SUI}}

Swiss Fliegertruppe

Specifications (AC-1)

{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|ref=
|crew=1
|length main= 23 ft 4¾ in
|length alt= 7.13 m
|span main= 39 ft 4½ in
|span alt= 12.o m
|height main= 10 ft 2¾ in
|height alt= 3.12 m
|area main= 258.34 ft²
|area alt= 24 m²
|empty weight main= 2,028 lb
|empty weight alt= 920 kg
|loaded weight main=
|loaded weight alt=
|max takeoff weight main= 2,910 lb
|max takeoff weight alt= 1320 kg
|engine (prop)=Gnome et Rhône licence-built Bristol Jupiter IX
|type of prop= radial piston
|number of props=1
|power main= 420 hp
|power alt= 313 kw
|max speed main= 152 mph
|max speed alt= 245 km/h
|range main= 280 miles
|range alt= 450 km
|ceiling main=
|ceiling alt=
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|power/mass main=
|power/mass alt=
|armament= intended to be two forward-firing machine guns
}}

References

{{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=}}

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