Hopfner HS-5/28
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| Hopfner HS-5/28 | |
|---|---|
| File:Walter NZ-60 a letadlo Hopfner HS-52.8.jpg Hopfner with engine Walter NZ-60 | |
| General information | |
| Type | Utility aircraft |
| National origin | Austria |
| Manufacturer | Hopfner |
| Designer | |
| Number built | 4 |
| History | |
| First flight | July 1928 |
The Hopfner HS-5/28 was a utility aircraft built in Austria in the late 1920s. It was a conventional, parasol-wing monoplane with seating for two occupants in tandem, open cockpits. The landing gear was of fixed, tailskid type with divided main units. Two examples were built with Walter NZ60 engines, followed by two more with the more powerful NZ85 for Swiss aeroclub use. One of these latter machines remained in service until 1934.
Variants
[edit | edit source]Specifications (HS-5/28)
[edit | edit source]Data from Jane's all the World's Aircraft 1928[1]
General characteristics
- Crew: 1
- Capacity: 1
- Length: 7.4 m (24 ft 3 in)
- Wingspan: 11.26 m (36 ft 11 in)
- Width: 3.1 m (10 ft 2 in) wings folded
- Height: 2.55 m (8 ft 4 in)
- Wing area: 19.8 m2 (213 sq ft)
- Empty weight: 385 kg (849 lb)
- Gross weight: 615 kg (1,356 lb)
- Max takeoff weight: 770 kg (1,698 lb)
- Powerplant: 1 × Walter NZ60 5-cylinder air-cooled radial piston engine, 45 kW (60 hp)
- Propellers: 2-bladed wooden fixed-pitch propeller
Performance
- Maximum speed: 148 km/h (92 mph, 80 kn)
- Landing speed: 50 km/h (31 mph; 27 kn)
- Range: 2,160 km (1,340 mi, 1,170 nmi) with maximum load
- Time to altitude: 1,000 m (3,300 ft) in 9 minutes
- Wing loading: 31 kg/m2 (6.3 lb/sq ft) normal; 38.8 kg/m2 (7.9 lb/sq ft)
- Power/mass: 17.16 kg/kW (28.2 lb/hp)
References
[edit | edit source]- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
Further reading
[edit | edit source]- Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).