Sukhoi Su-26M: Difference between revisions
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{{infobox Aircraft | {{infobox Aircraft | ||
|image = [[Image:Sf.png]] | |image = [[Image:Sf.png]] | ||
|name =Sukhoi Su-26M | |name = Sukhoi Su-26M | ||
|type = 1-engine piston | |type = 1-engine piston | ||
|livery = | |livery = | ||
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|fgname = <tt> Su-26M </tt> | |fgname = <tt> Su-26M </tt> | ||
|download = | |download = | ||
|features = 3D cockpit | |||
|features = smoke tracers | |||
}} | }} | ||
Revision as of 06:51, 13 November 2008
This article is a stub. You can help the wiki by expanding it. |
[[File:|300px|]] | |
Type | 1-engine piston |
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Author(s) | Enrique Laso Leon |
FDM | JSBSim |
--aircraft= |
/ Su-26M / Su-26M / Su-26M / Su-26M / Su-26M / Su-26M / Su-26M / Su-26M / Su-26M / Su-26M / Su-26M |
Status | alpha v1.0 |
Unlimited aerobatic aircraft designed by the Sukhoi OKB. The structure of the fuselage is a welded steel truss with fiber reinforced plastic panels. The wing has a CFRP (carbon fiber reinforced plastic) spar alleged to withstand 24g before breaking. The Su-26 replaced the Yak-55 family as the main soviet mount for international aerobatics competitions. The basic model was soon replaced by the more capable Su-26M (improved) and an export version was made available as the Su-26MKh (Su-26MX in cyrillic alphabet). The Su-26 was replaced by the even more capable Su-31 featuring a CFRP fuselage, a bubble canopy and optionally, a lightweight ejection seat. Another development is the 2-seat Su-29
Similar aircraft include the Extra 300, and Mudry CAP-232.
The Su-26MKh is depicted in the FG version with a 3-blade propeller and a 450HP M-14PF. The instrumentation is in metric system.