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Avia BH-6 & BH-8

BH-6

The Avia BH-6, an experimental fighter aircraft, was manufactured in Czechoslovakia in 1923.

This unique aircraft featured a single-bay biplane design and was developed alongside the BH-7, sharing similar fuselage and tail characteristics.

Notably, the BH-6 had wings of unequal span, with the top wing being shorter than the bottom wing.

The top wing was connected to the bottom wing through a single I-strut on each side, sloping inwards from bottom to top.

Unlike traditional designs, the top wing was not supported by cabane struts but rather by a single large pylon attached to the fuselage.

Unfortunately, both the BH-6 and the BH-7 experienced crashes during their testing phase, leading to the abandonment of this particular aircraft configuration.

BH-8

In 1923, Czechoslovakia introduced the Avia BH-8, a prototype fighter aircraft.

This aircraft was created as an improvement upon the BH-6 design, which had faced numerous challenges.

The BH-8 featured an unequal-span biplane structure and retained the unique wing cellule design of its predecessor.

Although the BH-8 showcased improved flying capabilities during its test flights, it ultimately lost its development momentum to the BH-17, another variant of the original design.

Specifications

BH-6

Crew

One

Length

6.47 m (21 ft 3 in)

Wingspan

9.98 m (32 ft 9 in)

Height

2.88 m (9 ft 5 in)

Wing area

22.6 m2 (243 sq ft)

Empty weight

878 kg (1,936 lb)

Gross weight

1,180 kg (2,601 lb)

Powerplant

1 × Skoda license-built Hispano-Suiza 8Fb,

224 kW (300 hp)

Performance

Maximum speed

220 km/h (137 mph, 119 kn)

Endurance

2 hours

Service ceiling

7,000 m (23,000 ft)

Armament

2 × fixed forward firing .303 Vickers machine guns.

Sources
Czechoslovakian Air Force, 1918-1970, Aircam Aviation Special 05-Richard Ward, Zdenek Titz & Gordon C. Davies.
Ceskoslovenské Letectvo, 1918-1924-Jiří Rajlich & Jiří Sehnal.

 

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