Hanriot H.35
Hanriot H.35 | |
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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]![](http://upload.wikimedia.org/wikipedia/commons/thumb/5/58/Hanriot_H.36_L%27A%C3%A9ronautique_January%2C1926.jpg/220px-Hanriot_H.36_L%27A%C3%A9ronautique_January%2C1926.jpg)
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.[2]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/c/c0/Hanriot_H.33_Les_Ailes_December_16%2C_1926.jpg/220px-Hanriot_H.33_Les_Ailes_December_16%2C_1926.jpg)
Specifications (H.35)
[edit]Data from [2]Illustrated Encyclopedia of Aircraft
General characteristics
- Crew: 2
- Length: 7.60 m (24 ft 11.25 in)
- Wingspan: 11.39 m (37 ft 4.5 in)
- Height: 2.70 m (8 ft 10.25 in)
- Wing area: 22.00 m2 (236.81 sq ft)
- Empty weight: 680 kg (1,499 lb)
- Gross weight: 945 kg (2,083 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, 100 kn)
- Range: 320 km (199 mi, 173 nmi)
- Service ceiling: 5,000 m (16,405 ft)
References
[edit]![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)
Wikimedia Commons has media related to Hanriot H.35.
Notes
[edit]Bibliography
[edit]- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.