Sukhoi Su-26 | |
|---|---|
| Riik | Nõukogude Liit |
| Tüüp | Aerobaatilised õhusõidukid |
| Esimene lend | Juuni 1984 |
| Ehitatud | Teadmata |
2007 Sukhoi Su-26 on endisest Nõukogude Liidust pärit ühekohaline aerobaatiline lennuk, mille jõuallikaks on üks radiaalne kolbmootor. Su-26-l on keskele paigaldatud sirged tiivad ja fikseeritud maandumisseade, mille peamine käik on paigaldatud tahkele titaankaarele.
Allikas: Sukhoi Su-26 Wikis
| Sukhoi Su-26M Walk Around | |
|---|---|
| Fotograafid | Vladimir Jakubov |
| Lokaliseerimine | Riiklik õhu- ja kosmosemuuseum - Udvar-Hazy keskus, Chantilly, VA |
| Fotod | 28 |
Sukhoi Su-26M 01
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Sukhoi Su-26M 08
Sukhoi Su-26M 07
Sukhoi Su-26M 09
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Vaata ka:
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) |
|---|---|
| Rolli | Unlimited Aerobatic Competition Aircraft |
| Tootja | Sukhoi Design Bureau / MAPO |
| First Flight (Su-26) | Juuni 1984 |
| Meeskonna | 1 pilot |
| Konfiguratsiooni | Mid-wing monoplane, conventional fixed gear |
| Empty Weight | 700 kg (1,540 lb) |
| Tiibade siruulatus | 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.
Vaadatud : 242
