Engineering:Aeris Naviter AN-2 Enara
| An-2 Enara | |
|---|---|
| Role | Helicopter |
| National origin | Spain |
| Manufacturer | Aeris Naviter |
| First flight | Pending |
| Introduction | 2009 |
| Status | Development ended (2012) |
The Aeris Naviter AN-2 Enara (Basque for 'Swallow') is a Spanish helicopter that was under development by Aeris Naviter of San Sebastián. The AN-2 was first shown at the 2009 Paris Air Show at Paris–Le Bourget Airport. The aircraft was intended to be supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1][2]
The AN-2 was intended to have certification completed in the European Aviation Safety Agency Very Light Rotorcraft category by May 2010, and then again by the end of 2012 but, by January 2013, this does not seem to have been completed. Kits were intended to be ready for delivery in February 2010, but were not yet available as of January 2013. By late in 2011 there was no indication that the prototype had been flown.[3][4]
By 2012 the company website was redirected to Cicare Europe and all mention of the AN-2 had been removed. It is likely development had ended by that point.[5]
Design and development
The AN-2 Enara features a two-rotor coaxial main rotor, a two-seats-in tandem enclosed cockpit, tricycle landing gear with suspension, an H-tail and a four-cylinder, four-stroke, 115 hp (86 kW) BMW automotive engine. Plans for other powerplants include the four cylinder, air-cooled, four-stroke, dual-ignition 115 hp (86 kW) Lycoming IO-233 light-sport aircraft engine.[1]
The aircraft fuselage is made from aluminium sheet. Its 6.99 m (22.9 ft) diameter two-bladed rotors both have chords of 18 cm (7.1 in). The aircraft has an empty weight of 390 kg (860 lb) and a gross weight of 600 kg (1,323 lb), giving a useful load of 210 kg (463 lb).[1]
Specifications (AN-2 Enara)
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Empty weight: 390 kg (860 lb)
- Gross weight: 600 kg (1,323 lb)
- Powerplant: 1 × BMW 1200 four cylinder, four stroke automotive engine, 86 kW (115 hp)
Performance
- Maximum speed: 170 km/h (110 mph, 92 kn)
- Cruise speed: 150 km/h (93 mph, 81 kn)
References
- ↑ 1.0 1.1 1.2 1.3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 189. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ Aeris Naviter (10 May 2009). "AN-2 Enara Rollout". http://www.aerisnaviter.com/en/new001.php. Retrieved 22 January 2013.[yes|permanent dead link|dead link}}]
- ↑ Aeris Naviter (n.d.). "AN-2 Enara". http://www.aerisnaviter.com/en/productPricesAN2.php. Retrieved 22 January 2013.
- ↑ Jane's Information Group (11 October 2011). "Aeris Naviter AN 2 Enara (Spain), Aircraft - Rotary-wing - Civil". http://articles.janes.com/articles/Janes-All-the-Worlds-Aircraft/Aeris-Naviter-AN-2-Enara-Spain.html. Retrieved 22 January 2013.
- ↑ Aeris Naviter (2009). "Aeris Naviter". aerisnaviter.com. Archived from the original on 23 December 2011. https://web.archive.org/web/20111223050741/http://www.aerisnaviter.com/en/main.html.
External links
- Official website archives on Archive.org
- Photo of the AN-2 Enara on Airliners.net
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