In 1969, the Soviet Union learned of the
U.S. Air Force's "F-X" program, which resulted in the
F-15 Eagle. The
Soviet leadership soon realised that the new American fighter would represent a serious technological advantage over existing Soviet fighters. "What was needed was a better-balanced fighter with both good agility and sophisticated systems." In response, the Soviet General Staff issued a requirement for a
Perspektivnyy Frontovoy Istrebitel (
PFI, literally "Prospective Frontline Fighter", roughly "Advanced Frontline Fighter"). Specifications were extremely ambitious, calling for long-range, good short-field performance (including the ability to use austere runways), excellent agility, Mach 2+ speed, and heavy armament. The aerodynamic design for the new aircraft was largely carried out by
TsAGI in collaboration with the
Sukhoi design bureau. The aircraft had a large wing, clipped, with two separate
podded engines and a
twin tail.
Air Force The first batch of flying prototypes were
T-10-1 and
T-10-2. They were powered by
Lyulka AL-21 turbojets and had
ogival wings. The aerodynamic layout was found to be unsatisfactory during construction; this was verified starting with T-10-1's
maiden flight on 20 May 1977. The aircraft completed trials in November 1983 and donated to the
Soviet Air Force Museum in late-1985. T-10-2 first flew on 16 May 1978. On 7 July 1978, it crashed and killed the pilot; the aircraft exceeded its
G limit and
broke-up in flight after behaving unpredictably when the control stick was pulled back. The prototypes were initially called "
Ram-K" by Western intelligence; they were first spotted by Western satellite imagery at the
Flight Research Institute's (LII) "Ramenskoye" airfield at
Zhukovsky; they were later assigned the
NATO reporting name "Flanker-A".
Komsomolsk-on-Amur Aircraft Plant (KnAAPO) built second batch -
T-10-3 and
T-10-4 - starting in 1978. These were the first to be fitted with the intended powerplant, the
Lyulka AL-31 turbofan, and their engine nacelles were redesigned accordingly. T-10-3 was initially used for powerplant testing; it first flew on 23 August 1979 after being delayed by engine trouble. In 1982 and 1983, it performed land-based
STOBAR tests for
naval aviation. T-10-4 was used for avionics and armament testing with the
Mech radar. Tests with the T-10-4 and the later
T-10-10 revealed serious deficiencies with the Mech radar. KnAAPO built a third batch of "type T-10-5" AL-21-powered aircraft -
T-10-5,
T-10-6,
T-10-9,
T-10-10,
T-10-11 - for avionics tests.
T-10-6 was destroyed in October 1980 in a ground fire caused by a leaking fuel line. T-10-10 and T-10-11 performed radar, weapons control and targeting tests. These prototypes found that avionics weight, AL-31 fuel consumption, and aerodynamics failed to meet requirements. The aircraft underwent a major redesign. Sukhoi accepted greater cooperation from SibNIA, which conducted extensive
wind tunnel testing. Contemporary Western aircraft were examined for ideas. The new design -
T-10S - bore only a superficial resemblance to the T-10; the design was completed in 1980 and was the precursor to the production Su-27. The first batch of flying T-10S prototypes were
T-10-7 (or
T-10S-1) and
T-10-12 (or
T-10S-2). T-10-7 was used for handling, manoeuvring, and AL-31 tests; it had no radar or mission avionics. It first flew on 20 April 1981, and crashed on 3 September 1981 after a critical in-flight failure; the pilot
ejected and survived, but the project's chief was replaced and the flight engineer was
dismissed. T-10-12 was completed by KnAAPO in March 1981 for fire control testing. On 23 December 1981, it broke-up in flight and killed the pilot. Sukhoi's general designer was dismissed after the crash. KnAAPO produced additional batches in 1982 -
T-10-15,
T-10-17 to
T-10-22 - and 1983 -
T-10-23 to
T-10-27. T-10-17 was the first aircraft built to full production standard and first flew on 26 May 1982. In 1983, it landed after losing part of a wing and a tail fin from structural failure. T-10-21 crashed on 25 May 1984 after a structural failure of a leading edge flap; the pilot ejected and survived. The
T-10S-3 was modified and officially designated the
P-42, setting a number of
world records for time-to-height, beating those set in 1975 by a
similarly modified F-15 called "The Streak Eagle". The
P-42 "Streak Flanker" was stripped of all armament, radar and operational equipment. The fin tips, tail-boom and the wingtip launch rails were also removed. The composite radome was replaced by a lighter metal version. The aircraft was stripped of paint, polished and all drag-producing gaps and joints were sealed. The engines were modified to deliver an increase in thrust of , resulting in a
thrust-to-weight ratio of almost 2:1 (for comparison with standard example see
Specifications). The production
Su-27 (sometimes
Su-27S, NATO designation 'Flanker-B') began to enter
VVS operational service in 1985, although manufacturing difficulties kept it from appearing in strength until 1990. The Su-27 served with both the
V-PVO and Frontal Aviation. Operational conversion of units to the type occurred using the
Su-27UB (Russian for
Uchebno Boevoy - "combat trainer", NATO designation 'Flanker-C') twin-seat trainer, with the pilots seated in tandem. When the naval Flanker trainer was being conceived the Soviet Air Force was evaluating a replacement for the
Su-24 "Fencer" strike aircraft, and it became evident to Soviet planners at the time that a replacement for the Su-24 would need to be capable of surviving engagements with the new American F-15 and F-16. The Sukhoi bureau concentrated on adaptations of the standard
Su-27UB tandem-seat trainer. However, the Soviet Air Force favoured the crew station (side-by-side seating) approach used in the Su-24 as it worked better for the high workload and potentially long endurance strike roles. Therefore, the conceptual naval
side-by-side seated trainer was used as the basis for development of the
Su-27IB (Russian for
Istrebityel Bombardirovshchik - "fighter bomber") as an Su-24 replacement in 1983. The first production airframe was flown in early 1994 and renamed the
Su-34 (NATO reporting name 'Fullback').
Navy on approach Development of a version for the Soviet Navy designated
Su-27K (from
Korabyelny - "shipborne", NATO designation 'Flanker-D') commenced not long after the development of the main land-based type. Some of the T-10 demonstrators were modified to test features of navalized variants for carrier operations. These modified demonstrators led to specific prototypes for the Soviet Navy, designated "
T-10K". The T-10Ks had
canards, an
arresting hook and carrier landing avionics as well as a retractable inflight refueling probe. They did not have the landing gear required for carrier landings or folding wings. The first T-10K flew in August 1987 flown by the famous Soviet test pilot
Viktor Pugachev (who first demonstrated the
Cobra maneuver using an Su-27 in 1989), performing test takeoffs from a land-based
ski-jump carrier deck on the
Black Sea coast at
Saky in the
Ukrainian SSR. The aircraft was lost in an accident in 1988. At the time the naval Flanker was being developed the Soviets were building their first generation of
aircraft carriers and had no experience with
steam catapults and did not want to delay the introduction of the carriers. Thus it was decided to use a takeoff method that did not require catapults by building up full thrust against a blast deflector until the aircraft sheared restraints holding it down to the deck. The fighter would then accelerate up the deck onto a ski jump and become airborne. The production
Su-27K featured the required strengthened landing gear with a two-wheel nose gear assembly, folding
stabilators and wings, outer
ailerons that extended further with inner double slotted
flaps and enlarged
leading-edge slats for low-speed carrier approaches, modified
leading edge root extension (LERX) with canards, a modified ejection seat angle, upgraded fly-by-wire, upgraded hydraulics, an arresting hook and retractable inflight refuelling probe with a pair of deployable floodlights in the nose to illuminate the
tanker at night. The Su-27K began carrier trials in November 1989, again with Pugachev at the controls, on board the first Soviet aircraft carrier, called
Tbilisi at the time and formal carrier operations commenced in September 1991. Development of the naval trainer, called the
Su-27KUB (from
Korabyelny Uchebno-Boyevoy - "shipborne trainer-combat"), began in 1989. The aim was to produce an airframe with dual roles for the Navy and Air Force suitable for a range of other missions such as reconnaissance, aerial refuelling, maritime strike, and jamming. This concept then evolved into the
Su-27IB (
Su-34 "Fullback") for the Soviet Air Force. The naval trainer had a revised forward fuselage to accommodate a side-by-side cockpit seating arrangement with crew access via a ladder in the nose-wheel undercarriage and enlarged canards, stabilisers, fins and rudders. The wings had extra ordnance hardpoints and the fold position was also moved further outboard. The inlets were fixed and did not feature
foreign object damage suppression hardware. The central fuselage was strengthened to accommodate maximum gross weight and internal volume was increased by 30%. This first prototype, the T-10V-1, flew in April 1990 conducting aerial refuelling trials and simulated carrier landing approaches on the Tbilisi. The second prototype, the T-10V-2 was built in 1993 and had enlarged internal fuel tanks, enlarged spine, lengthened tail and tandem dual wheel main undercarriage. After the
collapse of the USSR in 1991,
Russia, the successor state, started development of advanced variants of the Su-27 including the
Su-30,
Su-33, Su-34,
Su-35, and
Su-37. Since 1998, the export
Su-27SK has been produced as the
Shenyang J-11 in China under licence. The first licensed-production plane,
assembled in Shenyang from Russian supplied kits, was flight tested on 16 December 1998. These licence-built versions, which numbered 100, were designated J-11A. The next model, the J-11B made extensive use of Chinese developed systems within the
Su-27SK airframe. Starting in 2004, the Russian Air Force began a major update of the original Soviet Su-27 ('Flanker-B') fleet. The upgraded variants were designated
Su-27SM (Russian for "
Seriyniy
Modernizovanniy" - literally "
Serial
Modernized"). This included upgrades in air-to-air capability with the
R-77 missile with an active radar homing head. The modernized Su-27SM fighters belong to the
4+ generation. The strike capability was enhanced with the addition of the
Kh-29T/TE/L and
Kh-31P/Kh-31A ASM and
KAB-500KR/KAB-1500KR smart bombs. The avionics were also upgraded. The Russian Air Force is currently receiving aircraft modernized to the SM3 standard. The aircraft's efficiency to hit air and ground targets has increased 2 and 3 times than in the basic Su-27 variant. Su-27SM3 has two additional stations under the wing and a much stronger airframe. The aircraft is equipped with new onboard radio-electronic systems and a wider range of applicable air weapons. The aircraft's cockpit has multifunctional displays. The Su-30 is a two-seat multi-role version developed from the
Su-27UBK and was designed for export and evolved into two main variants. The export variant for China, the
SU-30MKK ('Flanker-G') which first flew in 1999. The other variant developed as the export version for India, the
Su-30MKI ('Flanker-H') was delivered in 2002 and has at least five other configurations. The Su-33 is the Russian Navy version of the Soviet
Su-27K which was redesignated by the Sukhoi Design Bureau after 1991. Both have the NATO designation 'Flanker-D'. The Su-34 is the Russian derivative of the Soviet-era
Su-27IB, which evolved from the Soviet Navy
Su-27KUB operational conversion trainer. It was previously referred to as the
Su-32MF. The newest and most advanced version of the Su-27 is the
Su-35S ("
Serial"). The Su-35 was previously referred to as the
Su-27M,
Su-27SM2, and
Su-35BM. The Su-37 is an advanced technology demonstrator derived from Su-35 prototypes, featuring thrust vectoring nozzles made of
titanium rather than steel and an updated airframe containing a high proportion of
carbon-fibre and
Al-Li alloy. Only two examples were built and in 2002 one crashed, effectively ending the program. The Su-37 improvements did however make it into new Flanker variants such as the
Su-35S and the
Su-30MKI. == Design ==