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Sukhoi Su-26


Single-Seat, Single-Engine Aerobatic Aircraft [ 1984 ]



The Sukhoi Su-26, a Soviet product of the late Cold War years, is a proven aerobatic performer and has spawned the Su-29 and Su-31 lines.



Authored By: Staff Writer | Last Edited: 03/19/2022 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

GO TO SPECIFICATIONS [+]
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The Sukhoi Su-26 is a Soviet-era lightweight, aerobatic racer powered through a single, nose-mounted engine and piloted by a sole crew member. The design appeared through a first-flight in June of 1984 and has been in actively utilized ever since. Related developments include the Sukhoi Su-29 and Su-31 platforms revealed in 1991 and 1992, respectively.

The Su-26 relies on elegant, aerodynamically-efficient streamlining of its airframe, seating the pilot over midships under a large-area windscreen. The nose is long, restricting forward vision from the cockpit and the mainplanes also reduce visibility to the forward-sides of the aircraft. These members are straight in their general shaping with clipped tips and positioned slightly ahead of midships. The dorsal spine is raised and the entire fuselage tapers towards the short tail section which is capped by a single vertical fin and seats a pair of low-mounted horizontal planes. The "tail-dragger" undercarriage (with arced, titanium-based main legs) is of a simple lightweight design and remains fixed during flight - further reducing complexity and maintenance commitments.

The aircraft is powered by a single Vedeneyev M14P series 9-cylinder, air-cooled radial piston engine developing 360 horsepower and driving a three-bladed constant-speed propeller unit at the nose. Coupled with its streamlined design, this gives the aircraft a maximum speed of 280 miles-per-hour, a range out to 500 miles, and a service ceiling up to 13,000 feet. Cruising speeds are closer to 185 mph. Rate-of-climb is 3,500 feet-per-minute.

Since its inception, the Su-26 has been something of a showstopper with its exceptional performances. It claimed the 1986 World Aerobatics Championships in both men's and women's team categories and also finished first in the 2004 European Championships as well as the 2003 and 2005 Aerobatic World Championships.

The original 1980s form of the aircraft was flown with a simpler two-bladed propeller unit. Since then, the series has seen several notable modified / modernized variants appear: the Su-26M is an offshoot refined throughout and introduced a three-bladed propeller arrangement among other changes. The Su-26M3 variant brought about use of the M9F engine of 430 horsepower.©MilitaryFactory.com
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.
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Specifications



Service Year
1984

Origin
Soviet Union national flag graphic
Soviet Union

Status
ACTIVE
In Active Service.
Crew
1

Production
20
UNITS


National flag of Russia National flag of the Soviet Union Russia; Soviet Union
(OPERATORS list includes past, present, and future operators when applicable)


Length
22.3 ft
(6.80 m)
Width/Span
25.6 ft
(7.80 m)
Height
9.5 ft
(2.89 m)
Empty Wgt
1,543 lb
(700 kg)
MTOW
1,742 lb
(790 kg)
Wgt Diff
+198 lb
(+90 kg)
(Showcased structural values pertain to the base Sukhoi Su-26 production variant)
monoplane / low-mounted / straight, tapered
Monoplane
Design utilizes a single primary wing mainplane; this represent the most popular mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
Straight, Tapered
The planform uses straight mainplane members which taper towards the wing tips.
(Structural descriptors pertain to the base Sukhoi Su-26 production variant)
Installed: 1 x Vedeneyev M14P 9-cylinder air-cooled radial piston engine developing 360 horsepower and driving a three-bladed propeller unit at the nose.
Max Speed
280 mph
(450 kph | 243 kts)
Ceiling
13,123 ft
(4,000 m | 2 mi)
Range
497 mi
(800 km | 1,482 nm)
Rate-of-Climb
3,545 ft/min
(1,081 m/min)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the base Sukhoi Su-26 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
None.


Supported Types




(Not all ordnance types may be represented in the showcase above)
Su-26 - Base Series Designation; original form with two-bladed propeller unit; four airframes completed.
Su-26M - Modified model with three-bladed MTV-9 series composite propeller unit; revised tail surfaces for improved control.
Su-26M3 - Fitted with M9F engine of 430 horsepower.


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