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Sukhoi
Su-57
Russia's first operational fifth-generation stealth fighter, combining internal weapons bays, supercruise and thrust-vectoring super-maneuverability. Fielded in limited numbers to the Russian Aerospace Forces, with a single export customer to date.
Max speed
2,440 km/h
Range
3,500 km
Payload
10,000 kg
💲 Estimated unit cost, disputed/uncertain public figures
Full specifications
Performance
Speed, range, altitude and engagement capability.
- Max speed
Maximum level speed. For aircraft this is at optimal altitude; for ground vehicles, top road speed. Higher means faster response and better kinematic performance.
- 2,440 km/h 67th pct in class
- Max speed (Mach)
Maximum speed as a multiple of the speed of sound. Mach 2+ is typical for air-superiority fighters.
- 2 Mach 33th pct in class
- Range
Maximum distance: ferry range for aircraft, operational range for vehicles, maximum engagement distance for missiles. Higher means more standoff or persistence.
- 3,500 km 50th pct in class
- Combat radius
Distance an aircraft can fly, complete its mission and return without refueling. Roughly a third of ferry range.
- 1,500 km 58th pct in class
- Service ceiling
Maximum operating altitude. Higher gives energy advantage and sensor horizon.
- 20,000 m 83th pct in class
- Thrust-to-weight
Engine thrust divided by loaded weight. Above 1.0 the aircraft can accelerate going straight up.
- 1.08 58th pct in class
Firepower
Armament, payload and guidance.
- Main armament
Primary weapon: main gun, cannon or missile type.
- 30 mm GSh-30-1 cannon
- Hardpoints
External stations for weapons and pods. More means bigger and more flexible loadouts.
- 10 17th pct in class
- Weapons payload
Maximum ordnance weight the platform can carry. Higher means more strike capacity per sortie.
- 10,000 kg 75th pct in class
Protection
Armor, countermeasures and survivability.
- Countermeasures
Self-protection: chaff, flares, DIRCM, towed decoys, smoke dischargers, jammers.
- Himalayas EW suite, chaff, flares
- Signature reduction
Radar cross-section shaping, RAM coatings, IR suppression. Actual RCS values are classified.
- Low observable airframe shaping with radar-absorbent coatings and internal weapons bays
Physical
Dimensions, weight and crew.
- Length
Overall length including gun/probe where applicable.
- 20.1 m
- Wingspan
Wingtip-to-wingtip span.
- 13.95 m
- Height
Overall height. Lower profile is harder to spot and hit for ground vehicles.
- 4.74 m
- Empty weight
Weight without fuel, ammunition or crew.
- 18,500 kg
- Combat weight
Fully loaded weight. Lighter eases transport and bridging limits; heavier often means more armor.
- 35,000 kg
- Crew
Personnel required to operate. Fewer reduces exposure; autoloaders trade a loader for mechanical complexity.
- 1
Propulsion
Engine, power and fuel.
- Engine
Powerplant model and type.
- 2x Saturn AL-41F1 (Izdeliye 30 on later production) thrust-vectoring afterburning turbofans
- Engines
Number of engines. Twin-engine gives redundancy at higher cost.
- 2
- Thrust
Total engine thrust (with afterburner where applicable).
- 147 kN 75th pct in class
- Fuel capacity
Internal fuel volume.
- 10,300 L
- Propulsion type
Turbofan, turboshaft, diesel, gas turbine, solid-fuel rocket, ramjet…
- Turbofan
Sensors & avionics
Radar, sensor suite and datalinks.
- Radar
Primary radar. AESA (active electronically scanned array) is the current state of the art.
- N036 Byelka AESA (multi-array)
- Sensors
IRST, EO/IR turrets, laser designators, sniper pods, thermal sights.
- 101KS Atoll electro-optical suite, Himalayas EW suite, distributed aperture IRST
Program
Cost, production scale and operators.
- Unit cost
Approximate flyaway/unit cost where public. Defense pricing varies hugely by contract, offsets and configuration. Lower is cheaper.
- $50,000,000 91th pct in class
- Units built
Total production run. Higher means proven manufacturing, mature logistics and spares availability.
- 30 8th pct in class
- Operator countries
Number of countries operating the system. More operators means broader support ecosystem.
- 1 0th pct in class
Specifications compiled from public Sukhoi and reference sources ↗. Published defense figures are approximations — treat comparisons as directional. Last verified 2026-07-01.
Frequently asked questions
What is the top speed of the Sukhoi Su-57? +
The Sukhoi Su-57 has a maximum speed of 2,440 km/h.
What is the range of the Sukhoi Su-57? +
The Sukhoi Su-57 has a maximum range of 3,500 km.
What is the weapons payload of the Sukhoi Su-57? +
The Sukhoi Su-57 can carry up to 10,000 kg of weapons payload.
How much does the Sukhoi Su-57 weigh? +
The Sukhoi Su-57 has a combat weight of 35,000 kg.
How many crew does the Sukhoi Su-57 require? +
The Sukhoi Su-57 requires a crew of 1.
What is the main armament of the Sukhoi Su-57? +
The Sukhoi Su-57's primary weapon is the 30 mm GSh-30-1 cannon.
What engine does the Sukhoi Su-57 use? +
The Sukhoi Su-57 is powered by the 2x Saturn AL-41F1 (Izdeliye 30 on later production) thrust-vectoring afterburning turbofans.
What is the Sukhoi Su-57 used for? +
The Sukhoi Su-57 is a fighter aircraft typically used for air superiority, multirole combat, deep strike.
How many countries operate the Sukhoi Su-57? +
The Sukhoi Su-57 is operated by 1 countries.
How much does the Sukhoi Su-57 cost? +
The Sukhoi Su-57 has an approximate unit cost of 50,000,000 USD. Defense pricing varies by contract, offsets and configuration — treat this as directional.
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