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Sukhoi Su-26M: Difference between revisions
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{{infobox Aircraft | {{infobox Aircraft | ||
|image = | |image = | ||
|name =Sukhoi Su-26M | |name =Sukhoi Su-26M | ||
|type = 1-engine piston | |type = 1-engine piston | ||
| Line 8: | Line 8: | ||
|fdm =JSBsim | |fdm =JSBsim | ||
|status = alpha v1.0 | |status = alpha v1.0 | ||
|authors = | |authors = flying toaster | ||
|fgname = <tt> Su-26M </tt> | |fgname = <tt> Su-26M </tt> | ||
|download = | |download = | ||
}} | }} | ||
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-50 family as the main soviet mount for international aerobatics competition. | |||
The basic model was soon replaced by the more capable Su-26M (improved) and an export version was made available 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-26MX is depicted in the FG version with a 3-blade propeller and a 450HP M-14PF. | |||
The instrumentation is in metric system. | |||
== See also == | == See also == | ||