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[edit]

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

References[edit]

  1. ^ 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
  2. ^ https://www.aviafrance.com/hanriot-h-33-aviation-france-651.htm