Suchoj Su-26

Suchoj Su-26
Kraju	Radzieckiego
Typu	Samoloty akrobacyjne
Pierwszy lot	czerwiec 1984
Zbudowany	Niewiedzy

Tthe Suchoj Su-26 to jednomiejscowy samolot akrobacyjny z byłego Związku Radzieckiego, napędzany pojedynczym gwiazdowym silnikiem tłokowym. Su-26 ma środkowo zamontowane proste skrzydła i stałe podwozie, główne podwozie zamontowane na solidnym łuku tytanowym.

Źródła: Suchoj Su-26 na Wiki

Sukhoi Su-26M Walk Around
Fotografów	Władimir Yakubov
Lokalizacja	Narodowe Muzeum Lotnictwa i Przestrzeni Kosmicznej – Udvar-Hazy Center, Chantilly, Wirginia
Zdjęcia	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

Click on a photo and use the mouse scroll to view all photos

Czekaj, szukam dla Ciebie zdjęć Suchoj Su-26...

Zobacz też:

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)
Roli	Unlimited Aerobatic Competition Aircraft
Producent	Sukhoi Design Bureau / MAPO
First Flight (Su-26)	czerwiec 1984
Załogi	1 pilot
Konfiguracja	Mid-wing monoplane, conventional fixed gear
Empty Weight	700 kg (1,540 lb)
Rozpiętość	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.

Liczba wyświetleń : 250