Comte AC-1

from Wikipedia, the free encyclopedia
Comte AC-1
Alfred Comte AC-1.jpg
Type: single seat fighter
Design country:

SwitzerlandSwitzerland Switzerland

Manufacturer:

Alfred Comte

First flight:

April 2, 1927

Commissioning:

1927

Production time:

1927 to 1927

Number of pieces:

1 prototype

The Comte AC-1 was a single-seat fighter aircraft made by the Swiss manufacturer Alfred Comte in the 1920s.

Development history

The Swiss company Flugzeugbau Alfred Comte, which was founded in Horgen near Zurich, began aircraft construction in the early twenties with the license production of German designs. The company's first own attempt was the Comte AC-1, which was privately developed to meet a requirement of the Swiss air force for a single-seat fighter aircraft. The prototype, which flew for the first time on April 2, 1927, was a stripped high-wing aircraft with a rigid tail-tail landing gear, similar in design to the French Dewoitine D.9. The basic construction was made of metal, the wings and the tail surfaces were covered with fabric, but the fuselage had a light aluminum skin. A Gnome-Rhône radial engine served as the engine.

The testing and evaluation by the air force led to the fact that the prototype was bought for the military, but no further series machines were ordered. The wing designed by Comte was then replaced by that of the Dewoitine D.9 and this combination was used to set a Swiss altitude record on November 19, 1928.

Technical specifications

Parameter Data
crew 1
length 7.30 m
span 12.24 m
height 3.00 m
Wing area 25.00 m²
payload 503 kg
Empty mass 837 kg
Max. Takeoff mass 1'340 kg
Top speed 250 km / h
Service ceiling 9,000 m
Range 450 km
Engines Bristol Jupiter 9Abx Mk IV with 420 hp
Armament (provided) 2 forward-firing machine guns

Web links