Bernard H.52

H.52
Role	Floatplane fighter
National origin	France
Manufacturer	Société des Avions Bernard
First flight	16 June 1933
Number built	2

The Bernard H.52 was a French floatplane fighter aircraft of the 1930s. It was a single engine, single-seat monoplane built in the hope of being selected by the French Navy. Two prototypes were built, but no production followed.

Design and development

In late 1932, the Société des Avions Bernard proposed to build a floatplane fighter to meet the requirements of the French Navy for a shipboard fighter suitable for operation from the catapults of its Battleships and Cruisers. The Bernard design, the H.52, was a mid-winged monoplane based on its Bernard 260 landplane fighter, using the same wings, rear fuselage and tail surfaces as the earlier design. It was of all-metal construction, principally duralumin, with a monocoque fuselage and stressed skin cantilever wings that were integrally constructed with the centre fuselage. Leading edge slots and large flaps were fitted to the wing to lower its landing speed, while its undercarriage consisted of two main floats. A single supercharged Gnome-Rhône 9Kdrs radial engine powered the aircraft ^[1]^[2]^[3]

The first of two prototypes flew on 16 June 1933, with the second flying in 1934. No production followed, with Bernard choosing to develop a new fighter to meet the requirements of the French Navy, the Bernard H.110. This had a similar layout, with wooden wings and a more powerful engine fitted, but had no more success in attracting orders than the H.52, the French Navy eventually selecting the Loire 210.^[1]

Specifications

Data from The Complete Book of Fighters^[1]

General characteristics

Crew: 1
Length: 9.30 m (30 ft 6 in)
Wingspan: 11.50 m (37 ft 9 in)
Height: 4.27 m (14 ft 0 in)
Wing area: 18.2 m² (196 sq ft)
Empty weight: 1,480 kg (3,263 lb)
Gross weight: 1,888 kg (4,162 lb)
Powerplant: 1 × Gnome-Rhône 9Kdrs 9-cyliner air-cooled radial engine, 370 kW (500 hp)

Performance

Maximum speed: 328 km/h (204 mph; 177 kn) at 4,000 m (13,125 ft)
Stall speed: 61 km/h (38 mph; 33 kn) ^[2]
Range: 600 km (373 mi; 324 nmi)
Service ceiling: 8,500 m (27,887 ft) ^[2]
Time to altitude: 9 minutes to 4,000 m (13,125 ft)

Armament

Guns: 2× 7.5 mm Darne machine guns under wings

Notes

1 2 3 Green and Swanborough 1994, p. 62.
1 2 3 Flight 22 March 1934, p. 286.
↑ Flight 22 November 1934, p. 1245.

References

Green, William and Gordon Swanborough. The Complete Book of Fighters. New York, Smithmark, 1994. ISBN 0-8317-3939-8.
"New Aircraft:The Bernard 52 C I". Flight, 22 March 1934. p. 286.
"The Fourteenth Paris Airshow". Flight, 22 November 1934, pp. 1236–1250.

External links

Aviafrance

Aircraft produced by Adolphe Bernard, Société Industrielle des Métaux et du Bois (Ferbois) and Société des Avions Bernard

Adolphe Bernard	AB 1 AB 2 AB 3 AB 4

S.I.M.B.	AB.C1 AB 3M AB 3T V.1 V.2 V.3 AB 10 AB 10T AB 12 AB 14 AB 15 AB 16

S.A.B.	18 T 18 GR 181 GR 18 T Bis 190 T 191 T 191 GR 192 T 193 T 194 T 195 T 197 GR 20 30 T H.V.40 H.V.41 H.V.42 H.52 60 T 61 T 70 71 S-72 S-73 74 S 75 80 GR 81 GR 82 84 GR 86 H 110 HV 120 160 161 200 T 200 TS 201 T 205 T 207 T HV 220 260 HV 320 510 T V.4

This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.