FlyNano Nano
| Nano | |
|---|---|
| Error creating thumbnail: File missing The FlyNano Proto prototype on its first flight on 11 June 2012 | |
| General information | |
| Type | Single-seat seaplane, under 70kg |
| National origin | Finland |
| Manufacturer | FlyNano |
| Designer | Aki Suokas |
| Status | Production completed |
| Number built | one prototype |
| History | |
| Introduction date | 2011 |
| First flight | 11 June 2012 |
The FlyNano Nano is a Finnish electric single seat seaplane, designed by Aki Suokas and produced by FlyNano of Lahti. It was introduced at AERO Friedrichshafen in 2011 and the prototype Proto version first flew on 11 June 2012. When it was available the aircraft was supplied as a complete ready-to-fly-aircraft.[1][2][3][4]
By 2022 the company website domain was for sale and it is likely that the company ceased operations in about 2020.[5]
Design and development
[edit | edit source]The aircraft was designed to comply with the EC 216/2008 Annex 2 (j) rules for deregulated class under 70 kg (154 lb) empty weight. It features a joined wing box wing, a single-seat open cockpit without a windshield, a hull for water operations, but no wheeled landing gear and a single electric engine in tractor configuration mounted above the cockpit.[1][2][3][6]
The aircraft is made from carbon fibre. Its 4.8 m (15.7 ft) span wing has no flaps. The initial plan was to produce several models with different powerplant options, including a two-stroke powered ultralight, a high-powered racing model and an electric model. The company has more recently announced that only the electric model will be produced, citing that "it's quiet, efficient, eco-friendly and it's easy to maintain". The aircraft wing can be removed for storage or ground transportation.[1][2][6]
Specifications (Nano)
[edit | edit source]Data from Bayerl and FlyNano[1][6]
General characteristics
- Crew: one
- Length: 3.8 m (12 ft 6 in)
- Wingspan: 4.8 m (15 ft 9 in)
- Empty weight: 70 kg (154 lb)
- Gross weight: 200 kg (441 lb)
- Powerplant: 1 × electric motor
Performance
- Cruise speed: 140 km/h (87 mph, 76 kn)
- Service ceiling: 3,000 m (9,800 ft)
- Maximum glide ratio: 6:1
See also
[edit | edit source]Aircraft of comparable role, configuration, and era
References
[edit | edit source]- ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 54. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 56. Flying Pages Europe SARL, 2015. Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ a b 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).
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- ^ a b c Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).