Aeroprakt A-26 Vulcan: Difference between revisions
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| unit cost= [[US$]]25,500 (2001 kit price)<ref>{{cite web|title=Aeroprakt: The Russians Are Coming! (Or Are Those Planes Ukrainian?)|url=http://www.dreamwings.co.za/Foxbat/articles/Ultraflight_Sept01.htm|accessdate=13 Feb 2011}}</ref><!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
| unit cost= [[US$]]25,500 (2001 kit price)<ref>{{cite web|title=Aeroprakt: The Russians Are Coming! (Or Are Those Planes Ukrainian?) |url=http://www.dreamwings.co.za/Foxbat/articles/Ultraflight_Sept01.htm |accessdate=13 Feb 2011 |deadurl=yes |archiveurl=https://web.archive.org/web/20100703014822/http://www.dreamwings.co.za/Foxbat/articles/Ultraflight_Sept01.htm |archivedate=2010-07-03 }}</ref><!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
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| developed from=[[Aeroprakt A-20]] |
| developed from=[[Aeroprakt A-20]] |
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| variants with their own articles=[[Aeroprakt A-36 Vulcan]] |
| variants with their own articles=[[Aeroprakt A-36 Vulcan]] |
Revision as of 13:33, 27 June 2017
Aeroprakt A-26 Vulcan | |
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A-26 Vulcan in flight | |
Role | Light twin |
National origin | Ukraine |
Manufacturer | Aeroprakt |
Designer | Yuri Yakovlev |
Developed from | Aeroprakt A-20 |
Variants | Aeroprakt A-36 Vulcan |
The Aeroprakt A-26 Vulcan is a light twin engine aircraft developed from a modified Aeroprakt A-20 light single aircraft. Some models imported to the United States are registered as Spectrum Aircraft SA-26 Vulcan.
Design and development
The A-26 has an extra 3° degree sweepback of the wings from its single engine counterpart, the A-20. The aircraft is powered by two Rotax 503 (eventually Rotax 582) engines in a pusher configuration.[1]
Operational history
An example of the A-26 was demonstrated at the 2000 Experimental Aircraft Association AirVenture airshow in Oshkosh, Wisconsin.[2] Spectrum Aircraft imported versions for the American market.[3]
Variants
The Aeroprakt A-36 Vulcan is an updated factory built Rotax 912S powered twin.[4]
Specifications (variant specified)
Data from Aeroprakt
General characteristics
- Capacity: 2
- Length: 6.7 m (22 ft 0 in)
- Wingspan: 11.4 m (37 ft 5 in)
- Height: 1.9 m (6 ft 3 in)
- Wing area: 15.7 m2 (169 sq ft)
- Empty weight: 290 kg (639 lb)
- Gross weight: 520 kg (1,146 lb)
- Fuel capacity: 38 l
- Powerplant: 2 × Rotax 582 , 48 kW (65 hp) each
Performance
- Maximum speed: 180 km/h (110 mph, 97 kn)
- Cruise speed: 130 km/h (81 mph, 70 kn)
- Stall speed: 65 km/h (40 mph, 35 kn)
- Rate of climb: 10 m/s (2,000 ft/min) 2.5 m/s with one engine
References
External links
![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)