Hanriot H.35

From Wikipedia, the free encyclopedia
Jump to: navigation, search


Hanriot H.35
Role Intermediate training monoplane
National origin France
Manufacturer Avions Hanriot
Number built 12+

The Hanriot H.35 was a 1920s French intermediate training monoplane designed and built by Avions Hanriot.[1][2]

Design and development[edit]

The H.35 was developed from the earlier H.34 basic trainer and was a two-seat strut-braced parasol monoplane.[1] The H.35 was powered by a 180 hp (134 kW) Hispano-Suiza 8Ab piston engine.[2] Twelve aircraft were built for use with the Hanriot flying school and also the Societe Francaise d'Aviation at Orly.[2]

A 1925 development of the H.35 was the H.36 which was a twin-float equipped version powered by a 120 hp (89 kW) Salmson 9Ac piston engine.[2] An order for 50 H.36s was placed by Yugoslavia but it is not known if any were delivered.[2]

Specifications (H.35)[edit]

Data from [2]Illustrated Encyclopedia of Aircraft

General characteristics

  • Crew: 2
  • Length: 7.60 m (24 ft 11¼ in)
  • Wingspan: 11.39 m (37 ft 4½ in)
  • Height: 2.70 m (8 ft 10¼ in)
  • Wing area: 22.00 m2 (236.81 ft2)
  • Empty weight: 680 kg (1499 lb)
  • Gross weight: 945 kg (2083 lb)
  • Powerplant: 1 × Hispano-Suiza 8Ab water-cooled eight-cylinder Vee piston engine, 134 kW (180 hp)

Performance

  • Maximum speed: 185 km/h (115 mph)
  • Range: 320 km (199 miles)
  • Service ceiling: 5000 m (16405 ft)

References[edit]

Notes[edit]

  1. ^ a b "Hanriot". Flight: 26–49. 2 December 1926. 
  2. ^ a b c d e f Orbis 1985, p. 2080

Bibliography[edit]