Bernard 70 Series
Bernard 74
Role	Racing and Fighter monoplanes Type of aircraft
National origin	France
Manufacturer	Bernard
First flight	1930 (Bernard 72)
Number built	3

The Bernard 70 was a 1920s design for a French single-seat monoplane fighter aircraft by the Société des Avions Bernard. It was not built but was developed into a racing monoplane designated the Bernard S-72, (later Bernard S-73). It was further developed into single-seat fighters, the Bernard 74-01 and Bernard 74-02, although only two of the fighters were built.

Design and development

The Bernard S-72 was a wooden stressed skin constructed cantilever low-wing monoplane powered by a Gnome-Rhône 5Bc^[1] radial engine and had a fixed tailskid landing gear.^[2] Flown by Paillard, the Bernard S-72 participated in the 1930 Coupe Michelin race. On 29 June, he took off from Le Bourget, landed successively in Reims, Nancy, Strasbourg, Dijon and Clermont-Ferrand, but unfortunately had to retire near Lyon as a result of engine failure.^[1] The S-72 was re-engined with a Gnome-Rhône 7Kb^[3] and re-designated the Bernard S-73. The S-73 was then developed into the Bernard 74 single-seat fighter and retained the Titan-Major engine.^[2] Two prototypes were built with the first flying in February 1931, powered by a 280 hp (kw) Gnome-Rhône 7Kbs radial engine,^[4] the second was fitted with a 268 kW (360 hp) Gnome-Rhône 7Kd engine and first flew in October 1931.^[1] The first prototype 74 was re-engined with a Gnome-Rhône 9Kbrs radial engine and re-designated the Bernard 75 it was later used as a pilot-trainer.^[2] No further aircraft were built.

Variants

Bernard 70

Unbuilt design for a single-seat fighter.^[2]

Bernard S-72

Single-seater racing monoplane powered by a 179 kW (240 hp) Gnome-Rhône 5Bc radial engine, first flight in May 1930 Later converted to the Bernard S-73.^[1][2]

Bernard S-73^[3]

The Bernard 72 re-engined with a 224 kW (300 hp) Gnome-Rhône 7Kb radial engine, first flown in May 1930.^[2][3]

Bernard 74-01

Single-seat fighter variant, powered by a 209 kW (280 hp) Gnome-Rhône 7Kbs radial engine, later converted to the Bernard 75.^[2][4]

Bernard 74-02

A second prototype powered by a 268 kW (360 hp) Gnome-Rhône 7Kd, first flown on 21 October 1931^[1]

Bernard 75

Prototype Bernard 74-01 fighter re-engined with a 373 kW (500 hp) Gnome-Rhône 9Kbrs radial engine and later used as a pilot-trainer.^[2][5]

Specifications (Bernard 74.01)

Data from ^[2][4]

General characteristics

• Crew: 1
• Length: 6.72 m (22 ft 0 in)
• Wingspan: 9.20 m (30 ft 2 in)
• Height: 2.50 m (8 ft 3 in)
• Wing area: 13.45 m² (145 sq ft)
• Empty weight: 825 kg (1,819 lb)
• Max takeoff weight: 1,106 kg (2,438 lb)
• Powerplant: 1 × Gnome-Rhône 7Kbs radial piston engine, 209 kW (280 hp)
• Propellers: 2-bladed

Performance

• Maximum speed: 310 km/h (193 mph, 104 kn)
• Service ceiling: 8,000 m (26,247 ft)

Armament

• Guns: Two fixed 7.7mm (0.303in) synchronised Vickers machine-guns

References

Notes

Bibliography

• Bruner, Georges (December 1972). "Bernard 72, 73, 74C.1". Le Album de Fanatique de l'Aviation (in French) (39): 7–10. ISSN 0757-4169.
• Liron, Jean (1990). Les avions Bernard. Collection Docavia. Vol. 31. Paris: Éditions Larivière. ISBN 2-84890-065-2.
• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.

External links

Wikimedia Commons has media related to Bernard 75.

• Bernard S-72
• Bernard S-73
• Bernard 74-01
• Bernard 74-02
• Bernard 75