Engineering:Hanriot H.33
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H.33 | |
---|---|
[1] | |
Role | Two seat fighter aircraft |
National origin | France |
Manufacturer | Avions Hanriot |
First flight | 1926 |
Number built | 1 |
The Hanriot H.33 was a French biplane 2-seat fighter aircraft built in 1926, derived from the Hanriot H.31. It was not successful and only one prototype was completed.
Specifications
Data from [2]
General characteristics
- Crew: Two
- Length: 7.56 m (24 ft 10 in)
- Wingspan: 12.58 m (41 ft 3 in)
- Height: 3.50 m (11 ft 6 in)
- Wing area: 38.50 m2 (414.4 sq ft)
- Empty weight: 1,122 kg (2,474 lb)
- Gross weight: 1,893 kg (4,173 lb)
- Powerplant: 1 × Salmson 18Ab 18-cylinder 2-row water-cooled in-line radial engine, 370 kW (500 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 235 km/h (146 mph, 127 kn)
- Range: 580 km (360 mi, 310 nmi)
- Service ceiling: 8,000 m (26,000 ft)
Armament
- Guns: *2 × fixed, forward firing synchronised 7.7 mm (0.303 in) Vickers machine guns in the forward fuselage
- 2 × fixed, forward firing 7.5 mm (0.295 in) Darne machine guns in the port and starboard wings
- 2 x flexibly mounted 7.7 mm (0.303 in) Lewis guns in the rear cockpit
References
- ↑ The image (File:Hanriot H.33 Les Ailes December 16, 1926.jpg) on commons is NOT an H.33 it is a Hanriot H.35
- ↑ "Hanriot H-33 - avion de chasse - Un siècle d'aviation française". Aviafrance.com. 1998-11-15. https://www.aviafrance.com/hanriot-h-33-aviation-france-651.htm. Retrieved 2022-08-31.
![]() | Original source: https://en.wikipedia.org/wiki/Hanriot H.33.
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