Engineering:Rud Aero RA-2
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Revision as of 23:52, 10 April 2022 by imported>John Stpola (linkage)
Short description: American aerobatic aircraft
| RA-2 | |
|---|---|
| |
| Role | Unlimited Aerobatic |
| National origin | United States |
| Manufacturer | Rud Aero |
| First flight | December 2012 |
The Rud Aero RA-2 is an United States , all carbon fiber, unlimited aerobatic aircraft built by Rud Aero in the Experimental-Exhibition category.[1][2]
Design and development
The RA-2 is a single engine, tandem seat, low-wing, conventional landing gear equipped aircraft, made out of carbon fiber. It uses a constant chord symmetrical airfoil. It has interchangeable aerobatic and cross-country wings.[2][3]
Variants
- RA-2
- Base model
- RA-2T Trainer
- Training model
- RA-3
- Two-seat trainer model[2]
Specifications (RA-2)
Data from EAA
General characteristics
- Crew: 1
- Capacity: 1
- Powerplant: 1 × Lycoming AEIO-580 Horizontally opposed piston, 320 hp (240 kW)
- Propellers: 4-bladed
Performance
- g limits: +- 13G
References
- ↑ "Rud Aero Expands". http://www.sebastianairport.com/index.php?option=com_content&view=article&id=42:v-raptor-comes-to-sebastian&catid=3:news&Itemid=38. Retrieved 25 August 2013.
- ↑ 2.0 2.1 2.2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015–16, page 124. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- ↑ "RA-2". Archived from the original on 25 August 2013. https://archive.today/20130825214532/http://rud.aero/our-aircraft/ra-2-unlimite-aerobatic-aircraft/. Retrieved 25 August 2013.
External links
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