Engineering:Hanriot H.35
From HandWiki
| Hanriot H.35 | |
|---|---|
| |
| Role | Intermediate training monoplane |
| National origin | France |
| Manufacturer | Avions Hanriot |
| Number built | 12+ |
The Hanriot H.35 was a 1920s France intermediate training monoplane designed and built by Avions Hanriot.[1][2]
Design and development
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]
another view of the H.35[3]
Specifications (H.35)
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
Notes
Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
 |  |
