Sukhoi Su-26 | |
|---|---|
| Pays | Union soviétique |
| Type | Avions de voltige |
| Premier vol | Juin 1984 |
| Construit | Inconnu |
Lla Sukhoi Su-26 est un avion de voltige monoplace de l’ex-Union soviétique, propulsé par un seul moteur à pistons radiaux. Le Su-26 a des ailes droites montées au milieu et un train d’atterrissage fixe, le train principal monté sur un arc en titane solide.
Source: Sukhoi Su-26 sur Wiki
| Sukhoi Su-26M Walk Around | |
|---|---|
| Photographes | Vladimir Yakubov |
| Localisation | Musée national de l’air et de l’espace – Centre Udvar-Hazy, Chantilly, VA |
| Photos | 28 |
Sukhoi Su-26M 01
Sukhoi Su-26M 02
Sukhoi Su-26M 03
Sukhoi Su-26M 04
Sukhoi Su-26M 05
Sukhoi Su-26M 06
Sukhoi Su-26M 08
Sukhoi Su-26M 07
Sukhoi Su-26M 09
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General Characteristics
The Sukhoi Su-26M is a single-seat, single-engine aerobatic aircraft derived from the original Su-26. It is one of the world’s premier unlimited-class aerobatic competitors, known for its extremely light weight, high power-to-weight ratio, and robust structure capable of withstanding severe g-forces.
| Property | Value (Su-26M) |
|---|---|
| Rôle | Unlimited Aerobatic Competition Aircraft |
| Fabricant | Sukhoi Design Bureau / MAPO |
| First Flight (Su-26) | Juin 1984 |
| Crew | 1 pilot |
| Configuration | Mid-wing monoplane, conventional fixed gear |
| Empty Weight | 700 kg (1,540 lb) |
| Envergure | 7.80 m (25 ft 7 in) |
Design and Powerplant
- Engine: One Vedeneyev M-14P 9-cylinder, air-cooled radial piston engine.
- Power Output: 268 kW (360 hp).
- Propeller: Three-bladed (later four-bladed) German Mühlbauer composite propeller.
- Construction: The Su-26 was the first Soviet aerobatic aircraft to use over 50% composite materials, resulting in a very high strength-to-weight ratio.
- Fuselage: Steel tube truss structure, titanium in critical areas.
- Cockpit: Bubble canopy provides excellent all-around visibility, crucial for aerobatic competition.
Performance and Handling
- Maximum Speed: 450 km/h (280 mph).
- Stall Speed: 105 km/h (65 mph).
- Roll Rate: Extremely high, exceeding 360 degrees per second.
- G-Force Limits: Certified for maximum load factors of +12 to -10g, allowing for extremely violent maneuvers typical in international unlimited aerobatics.
- Key Improvement (Su-26M): The « M » variant introduced structural enhancements, redesigned wingtips, lighter materials, and often a four-bladed propeller, further enhancing its vertical performance and roll authority.
- Competition Success: The Su-26 family won numerous gold medals at World and European Aerobatic Championships, demonstrating superior performance against its Western counterparts.
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