at the
MAKS-2015 Air Show|alt= The Su-57 is a
fifth-generation multirole fighter aircraft and the first operational stealth aircraft for the Russian armed forces. In addition to stealth, the fighter emphasizes supermaneuverability in all aircraft axes, capacious internal payload bays for multirole versatility, and advanced sensor systems such as
active phased-array radar as well as the
integration of these systems to achieve high levels of automation. In the Su-57's design, Sukhoi cited the
Lockheed Martin F-22 as the baseline for a supermaneuverable stealth fighter, but addressed what the bureau considered to be the limitations, such as the inability to use thrust vectoring to induce roll and yaw moments, a lack of space for weapons bays between the engines resulting in insufficient payload, and complications for post-stall recovery if thrust vectoring fails. In particular, Sukhoi considered the F-22 design unsuitable as a multirole fighter required for PAK FA due to the limited payload that was too focused on air-to-air missiles. The aircraft has a wide
blended wing body fuselage with two widely spaced engines and has all-moving
horizontal and
vertical stabilisers, with the vertical stabilisers canted for stealth; the trapezoid wings have
leading edge flaps,
ailerons, and
flaperons. The aircraft incorporates
thrust vectoring and large
leading edge root extensions that shift the aerodynamic center forward, increasing static instability and maneuverability. These extensions have adjustable
leading–edge vortex controllers (LEVCONs) designed to control the generated vortices and can provide trim and improve high
angle of attack behaviour, including a quick stall recovery if the thrust vectoring system fails. To
air-brake, the ailerons deflect up while the flaperons deflect down and the vertical stabilisers toe inward to increase drag. Although the majority of the structural materials are
alloys with 40.5–44.5%
aluminum alloys and 18.6%
titanium alloys, the aircraft makes extensive use of
composites, with the material comprising 22–26% of the structural weight and approximately 70% of the outer surface. Designed from the outset as a multirole aircraft, the Su-57 has substantial internal payload capacity that allows the carriage of multiple large air-to-surface ordnance. The high degree of static instability (or
relaxed stability) in both pitch and yaw, advanced KSU-50
flight control system, and canted thrust
vectoring nozzles make the Su-57
departure-resistant and
highly maneuverable in all axes and enables the aircraft to perform very high angles of attack maneuvers such as the
Pugachev's Cobra and the
bell maneuver, along with doing flat rotations with little altitude loss. The aerodynamics and engines enable it to achieve speeds of Mach 2 and fly supersonic without afterburners, or
supercruise, at Mach 1.3, giving a significant kinematic advantage and extends the effective range of missiles and bombs over previous generations of aircraft. Combined with a high fuel load, the fighter has a supersonic range of over , more than twice that of the Su-27. An extendable refueling probe is available to further increase its range.
Stealth The first aircraft in Russian military service to emphasize stealth, the Su-57 employs a variety of methods to reduce its radar signature. Similar to other stealth fighters such as the F-22, the aircraft aligns the planform edges to reduce its
radar cross-section (RCS); the leading and trailing edges of the wings and control surfaces and the
serrated edges of
skin panels are carefully angled to reduce the number of directions the radar waves can be reflected. Weapons are carried internally in weapons bays within the airframe and antennas are recessed from the surface of the skin to preserve the aircraft's stealthy shape, while
radar absorbent material (RAM) coatings absorb radar emissions and reduce the reflection back to the source. The infrared search-and-track sensor housing is turned backwards when not in use and its rear is also treated with RAM. To mask the significant RCS contribution of the engine face, the walls of the inlet ducts are coated with RAM and the partial
serpentine ducts obscure most of the engines' compressor face and inlet guide-vanes (IGV); the remaining exposed engine face is masked by a slanted blocker grid placed in front of the IGV at a distance of 0.7–1.2 times the diameter of the duct, similar in principle to the method on the
Boeing F/A-18E/F. The aircraft canopy is coated with 70–90 nm thick metal oxide layers with enhanced radar wave absorbing to reduce the radar return of the cockpit by 30% and protect the pilot from the impact of ultraviolet and thermal radiation. The production tolerances are significantly tighter than previous Russian fighters in order to improve stealth characteristics. The combined effect of airframe shape and RAM of the production aircraft is estimated to have reduced the aircraft's RCS to a value thirty times smaller than that of the Su-27. Sukhoi's patent for the T-50 stealth features cites an intention to reduce average RCS to approximately 0.1 to 1 m2, compared to the Su-27's RCS of approximately 10 to 15 m2. The Su-57's design emphasizes frontal stealth, with RCS-reducing features most apparent in the forward hemisphere; the shaping of the aft fuselage is less optimized for radar stealth compared to American stealth designs such as the F-22 and
F-35, likely as a result of cost reduction as well as the Russian doctrine of operating the aircraft within the umbrella of friendly integrated
air defense systems. The aircraft has been scrutinized for the rough production quality, particularly on test aircraft often used for flight and static displays; production aircraft generally have better quality. On 4 November 2024, the fourth Su-57 prototype, T-50-4, was to be put on static display at China's
Zhuhai Airshow. Video taken of the aircraft, and uploaded to social media, highlighted a number of issues, including numerous screws and rivets that were "clearly visible" and not "flush" with the panels. Sections were described as "poorly aligned" with visible gaps between parts of the fuselage. The airframe wasn't designed for low observability and showed signs of "poor workmanship". The tail had different types of bolts used. Bolts with "single-slotted, Phillips, and with a hexagonal hex head". Rivets were used instead of bolts to reduce
radar cross section (RCS) compared to screws. By comparison, the F-35 has a RCS of "around 0.005 square meters", the F-22 has a RCS of "0.0005 square meters", and the Su-57 has a RCS of "0.1 to 0.5 square meters". The weapons bay door couldn't be fully closed.
Engines The Su-57 is powered by a pair of NPO Lyulka-Saturn
izdeliye 117, or AL-41F-1, augmented turbofans. The engine is a highly improved and uprated variant of the
AL-31 and produces 9 tonnes (88.3
kN, 19,840
lbf) of dry thrust, 14.5 tonnes (142.2 kN, 31,970 lbf) of thrust in afterburner, and 15 tonnes (147.1 kN, 33,070 lbf) of thrust in "special" emergency power. The engines have full authority digital engine control (
FADEC) and are integrated into the flight control system to facilitate maneuverability and handling. The aircraft employs
thrust vector control (TVC) where the vectoring nozzles' rotational axes are each canted at an angle, similar to the nozzle arrangement first employed on the
Su-30MKI and also used on Su-35S. The nozzles themselves vector in only one plane; the canting allows roll and yaw moments by vectoring each nozzle differentially, thus enabling the aircraft to produce thrust vectoring moments about all three aircraft axes,
pitch, yaw and roll. The engine inlet incorporates variable
intake ramps for supersonic efficiency and retractable mesh screens to prevent engine damage from
foreign object debris ingestion especially when operating in short, austere runways. The planned Su-57M will be equipped with a new engine from NPO Saturn in the mid-2020s under the development designation
izdeliye 30 and eventually designated AL-51F-1. The powerplant is designed with an estimated thrust of 11 tonnes (107.9 kN, 24,250 lbf) dry and 16.5 tonnes (162 kN, 36,380 lbf) in afterburner. In addition to improved performance, reliability, and costs compared to the AL-41F-1, the AL-51F-1 will also reduce the aircraft's radar and infrared signature with glass-fibre plastic IGVs and a new nozzle with serrated flaps. In 2023, it was reported that
UEC Saturn is developing an alternative non-axisymmetric "flat" nozzle for the Su-57; flight testing began in late 2024. Because the flat nozzle was requested well after Sukhoi had finalized the Su-57 design, Saturn designed the nozzle to fit with minimal changes to the airframe. In 2025, Rostec unveiled the
izdeliye 177 engine, which combines the technologies of both the AL-41F-1 and AL-51F-1; this engine produces 11 tonnes (107.9 kN, 24,250 lbf) dry and 16 tonnes (157 kN, 35,270 lbf) in afterburner. It first flew in December 2025. The main bays have two types of ejection launchers made by
Vympel, the UVKU-50L for missiles weighing up to , and the UVKU-50U for ordnance weighing up to ; the side bays use the VPU-50 launch rails. The primary medium-range missile is the active radar-homing
K/R-77M (
izdeliye 180), an upgraded R-77 variant with AESA seeker, dual-pulse motor, and conventional rear fins. A clean-sheet design short-range missile designated K-MD (
izdeliye 300) is being developed to eventually replace the R-74M2. For longer ranged applications, the Su-57 can carry the
izdeliye 810 missile, a further development of the
R-37M with shorter control surfaces and updated motor and seeker, with two in each main weapons bay; the R-37M could be carried externally. For striking surface targets, the aircraft can carry the KAB-250 or KAB-500
precision guided bombs in its main bays. Internal weapons also include the
Kh-38M air-to-ground missile,
Kh-35U (AS-20 "Kayak") anti-ship missile,
Kh-58UShK (AS-11 "Kilter")
anti-radiation missile, and
Kh-69 (originally designated Kh-59MK2) cruise missile. For missions that do not require stealth, the Su-57 can carry stores on its six external hardpoints which can use most Russian tactical fighter weapons. One of the new standoff cruise missiles designed for external carriage is the S-71K. According to the US, it is expected to be
nuclear-capable with a missile similar to the
Kh-47M2 Kinzhal. The missile is to have intra-body accommodation and smaller dimensions to allow it to be carried inside the Su-57's main bays. The aircraft has a 9A1-4071K (
GSh-30-1) 30 mm
autocannon with 150 cartridges mounted internally near the right LEVCON root. The weapon has an effective range of against aerial targets and against surface targets.
Cockpit The Su-57 has a
glass cockpit with no analogue gauges; information is displayed on two main multi-functional
LCD displays similar to the arrangement of the Su-35S. Supplementing the primary display is a smaller multi-functional display and digital control panel. The cockpit has a wide-angle (30° by 22°)
head-up display (HUD). Primary controls are the
joystick and a pair of throttles, with all major functions controlled with hands on throttle and stick (
HOTAS). The aircraft uses a two-piece
canopy, with the aft section sliding forward and locking into place. The canopy is treated with metallized coatings to reduce the aircraft's radar signature. The Su-57 integrated computer system at Chip "1890VM8Ya" – FGU FSC NIISI (in Russian). The aircraft uses the
NPP Zvezda K-36D-5 ejection seat and the SOZhE-50
life support system, which comprises the
anti-g and oxygen generating system. The pilot is equipped with a ZSh-10B helmet which mounts the NSTsI-50 digital display system, which enhances pilot situational awareness through pupil tracking and allows engagement of targets at high angles off-boresight. The oxygen generating system provides the pilot with unlimited oxygen supply. The life support system enables pilots to perform 9-g maneuvers for up to 30 seconds at a time, while the ejection seat and the new PPK-7
flight suit allows safe ejection at altitudes from 0 to and instrument airspeeds from 0 to ; the system also includes a survival kit to assist the pilot after ejection.
Avionics One of the main technical goals of the PAK FA programme is to achieve total integration of avionics systems, or sensor fusion, increase the pilot's situational awareness and reduce workload. Integration of the Su-57's onboard systems is controlled by an IUS (, ), with its computer system developed by GRPZ from
Ryazan. The main avionics systems are the
Sh-121 () multifunctional integrated radio electronic system (MIRES) and the
101KS "Atoll" () electro-optical system. In a departure from prior Sukhoi aircraft, the IUS systems integration was performed by Sukhoi itself rather than RPKB of Ramenskoye. The integrated avionics suite, called IMA BK (, ), uses fibre optic channels and runs on over 4 million
lines of code. The nose antenna is tilted backwards for stealth. Moreover, the side-looking radar could enable the Su-57 to employ beaming tactics while still able to guide its own missile. Redundant radio telephone communication and encrypted data exchange among various aircraft and also command centers (ground and sea-based and airborne) are provided by the S-111 system, developed by
Polyot. The
UOMZ 101KS "Atoll" electro-optical system consisted of the 101KS-V
infrared search and track (IRST), 101KS-O directional infrared counter measures (
DIRCM), 101KS-U
ultraviolet missile approach warning sensors (MAWS), 101KS-P thermal imager for low altitude flight and landing, and 101KS-N navigation and
targeting pod. The IRST turret is mounted on the starboard side in front of the cockpit and can track multiple targets simultaneously. When not in use, the receiver is turned backwards and its rear is treated with RAM to preserve stealth. Additionally, the Su-57 is the first fighter to mount a DIRCM system, with one turret mounted behind the canopy and another mounted under the cockpit. The aircraft is capable of deploying countermeasures such as flares and radar decoys, as well as single-use programmable ECM transmitters. The dispensers for these countermeasures are mounted in the tail boom between the engines. For in-flight navigation, the Su-57 uses the BINS-SP2M
inertial navigation system developed by
Concern Radio-Electronic Technologies (KRET). The system can also integrate with
GLONASS, and is controlled by the IVS-50 computing system. In 2016, KRET announced it is developing a multifunctional video processing system called "Okhotnik" (Hunter) to increase the Su-57's target detection range as well as to improve automatic detection and tracking of targets. A monitoring system allows real-time assessment of the aircraft's condition and predict the remaining 'life' of the composite parts of the aircraft by transmitting information through optical fibers, with sensitivity to mechanical influences, woven into the structure. This allows a more efficient maintenance and repair process. The Su-57 could also serve as a testbed for advanced AI and man-unmanned teaming technologies intended for use in a future
sixth-generation fighter program. The aircraft has also tested autonomous flight without pilot input. ==Operational history==