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Bernard 70

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Top speed
  
310 km/h

Length
  
6.72 m

Wingspan
  
9.2 m

First flight
  
1930

Manufacturer
  
Société des Avions Bernard

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.

Contents

Design and development

The Bernard S-72 was a wooden stressed skin constructed cantilever low-wing monoplane powered by a Gnome-Rhône 5Bc radial engine and had a fixed tailskid landing gear. 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. The S-72 was re-engined with a Gnome-Rhône 7Kb 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. Two prototypes were built with the first flying in February 1931, powered by a 280 hp (kw) Gnome-Rhône 7Kbs radial engine, the second was fitted with a 268 kW (360 hp) Gnome-Rhône 7Kd engine and first flew in October 1931. 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. No further aircraft were built.

Variants

Bernard 70
Unbuilt design for a single-seat fighter.
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.
Bernard S-73
The Bernard 72 re-engined with a 224 kW (300 hp) Gnome-Rhône 7Kb radial engine, first flown in May 1930.
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.
Bernard 74-02
A second prototype powered by a 268 kW (360 hp) Gnome-Rhône 7Kd, first flown on 21 October 1931
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.

Specifications (Bernard 74.01)

Data from

General characteristics

  • Crew: 1
  • Length: 6.72 m (22 ft 1 in)
  • Wingspan: 9.20 m (30 ft 2 in)
  • Height: 2.50 m (8 ft 2 in)
  • Wing area: 13.45 m2 (144.8 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; 167 kn)
  • Service ceiling: 8,000 m (26,247 ft)
  • Armament

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

    Bernard 70 Wikipedia