Su-33 – Originally designated the Su-27K, this variant is specifically designed for the demanding
role of carrier-based aviation. Equipped with canards for improved take off and landing performance, the first Su-27K made its maiden flight in 1985. The shortened tailcone, intended to
reduce risk of tail strike during high AOA landing, reduces the space for defensive equipment
(including chaff and flare dispensers). Whereas the Su-27 was tailored primarily as an air-to-air
interceptor, the Su-33 is a multi-role aircraft (a necessity of carrier based aviation operating far
from home bases). The Su-33 retains to a large extent the avionics and cockpit of the basic Su-27.
Su-34 – Also known as the Su-32FN, this aircraft is a two-seat (side by side cockpit), longrange, day/night fighter-bomber, intended to replace the MiG-27, Su-17, and Su-24. The Su-34
first flew on December 18, 1993. Canards improve manoeuvreability, and an elongated tailcone
reportedly houses aft facing missile guiding systems. The aircraft features an improved glass cockpit along with the traditional analog gauges. Besides having a unique ejection system and terrain
following radar, the aircraft actually has a toilet and sleeping facilities onboard.
Su-35 – Originally designated the Su-27M, this multi-role variant of the Su-27 features improved
avionics; a modern “glass cockpit” replacing the traditional analog gauges with multi-function displays and digital readouts. The collapse of the Soviet Union has hindered the deployment of the
Su-35, prototypes of which perform routinely at international airshows.
Su-37 – Having appeared at numerous airshows, this variant is basically an Su-35 equipped with
thrust vectoring engine exhausts for improved low-speed agility. Russia has stated that this will
eventually become the standard operating variant.
Ready For Action
This concludes our introduction to the Flanker family, arguably the most powerful and versatile
group of aircraft ever built. Chapter 2 will orient you with the simulation interface and explain how
to get airborne quickly.
CHAPTER 1: Flanker Briefing 3
The program, though, quickly began to experience problems. The second prototype, number T-102, suffered control system failure, and the pilot was killed during ejection. By 1979, additional prototypes were flying, but the program was failing to meet its performance requirements. Drag was
higher than expected, engine performance was low, fuel consumption was too high, and heavy
avionics in the nose decreased stability. Further, flutter problems required the addition of anti flutter weights in the tailfins, tailplanes, and wings. By this time, information about the F-15 indicated
the Flanker would be no match for the American jet in air-to-air combat. A redesign was needed.
Prototypes T-10-7 and T-10-8 were redesignated T-10S-1 and T-10S-2 and built to a substantially
improved design. An entirely new wing improved lift while offsetting the weight of the equipmentpacked nose. Anti-flutter weights, serving as wingtip missile launch rails, replaced the curved
wingtips of the early prototypes. The fuselage received substantial modifications, fins were
increased in size, and the airbrake was redesigned. The T-10S-1 first flew in 1981. Avionics problems continued to dog the program, though, and service deliveries didn’t begin until 1985, roughly
a decade after the F-15 entered service. One of the T-10S prototypes, redesignated as P-42, was
prepared to capture numerous aviation records from the F-15. Stripped of avionics and unnecessary gear, the P-42 was fitted with modified engines and set a total of 27 world records between
October 1986 and December 1988, including numerous time-to-height records.
Performance Characteristics
T-10-1 SU-27 SU-33 SU-34 SU-35
Powerplant
2 x AL-21F3 2 x AL-31F 2 x AL-35F 2 x AL35F 2 x AL-35F or AL-31MF
or AL-31MF or AL-31MF
Thrust Each Engine
11,220kg 12,522kg 14,029kg 14,029kg 14,029kg
Wingspan
14.8m 14.8m 14.8m 14.8m 15.1m
Height
5.92m 5.98m 5.95m 5.95m 6.42m
Max Takeoff Weight
25,786kg 30,000kg 30,000 kg. 44,400kg
Flanker Variants
Most legendary tactical aircraft share a common trait: versatility. The Flanker is no exception, with
numerous sub-variants arriving on the scene. Usually, aircraft variants are identified by adding a
letter to the base designation (F-16A, F-16B, F-16C, etc.), Sukhoi eventually abandoned this
method, giving each variant a new designation. Some speculate that this was intended to promote
the idea that each variant was a whole new aircraft, hopefully improving domestic funding as well
as overseas sales. Flanker operators include Belarus, Ukraine, Russia, India and China.
Su-30 – Initially called the Su-27PU, this is an improved version of the original Su-27UB two-seat
trainer. Unlike the Su-27UB, the Su-30 is a fully operational combat aircraft. It is optimized for missions lasting 10 or more hours, and would normally act as an airborne mission controller.
Su-30MK - This improved version of the Su-30 is optimized for delivery of precision-guided
munitions, some of which may have stand-off ranges of 120km (75 miles). The Su-30MK also features an improved navigation and weapons systems.
FLANKER 2.0
FLANKER 2.0
2 CHAPTER 1: Flanker Briefing