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Hanriot H.33

From Wikipedia, the free encyclopedia
H.33
[1]
RoleTwo seatfighter aircraft
Type of aircraft
National originFrance
ManufacturerAvionsHanriot
First flight1926
Number built1

TheHanriot H.33 was a Frenchbiplane 2-seatfighter aircraft built in 1926, derived from theHanriot 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-lineradial 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 aHanriot H.35
  2. ^"Hanriot H-33 - avion de chasse - Un siècle d'aviation française". Aviafrance.com. 1998-11-15. Retrieved2022-08-31.
Hanriot aircraft
Pre-1916, including some Ponnier types
Hanriot (Dupont) 1916-30
Lorraine-Hanriot 1930-33, Hanriot 1933-37 and SNCAC 1937-40
Retrieved from "https://en.wikipedia.org/w/index.php?title=Hanriot_H.33&oldid=1107788360"
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