ARMSNET
Military Equipment Database
Initializing 0%

Su-57

Su-57

Multi-Role Fighters
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
Su-57
Designation
Su-57
Alternate Designation
Su-57 Felon
Equipment Type
Multi-Role Fighters
Manufacturer
UAC, NAPO, Sukhoi
Date of Introduction
2025
Description

The Future Tactical Aviation Concept (PAK FA or Prospective/Promising Aircraft System of the Frontline Aviation) was disclosed by the Russian Air Force in early 2002 as the program aimed at providing the fifth generation fighter. The PAK FA stealth fighter aircraft will have a maximum takeoff weight of 35 tons and a combat radius of more than 1,700 kilometers. It will be fitted with integrated avionics, state-of-the-art sensors and new weaponry. The estimated cost of each airplane will not exceed $30 million (equivalent ot USD in year 2002) being affordable for many export customers and the Russian Air Force. The T-50 prototype was powered by the 117S engine developed for the Su-35 4+ generation fighter aircraft. The eight T-50 prototypes are being used for testing technologies, engineering solutions, weapons and sensors that will available for the production combat aircraft. In early 2006, The Russian Air Force stated that the PAK FA first prototype, called the I-21, maiden flight was planned for the end of 2006 after surpassing wind tunnel tests. The aircraft's avionics and engines were already on display during Moscow Air Show in 2005. In August 2007, the Russian Ministry of Defense stated that the first pre-production aircraft would be assembled in the near future and would take to the air in 2008. The PAK FA development cost has been estimated at $20 billion In a statement released on September 29, 2008, in New Delhi both India and Russia agreed on the development of two versions of the fifth-generation fighter. The Russian version will be a single-seat fighter while Indian version will be a two-seat aircraft featuring a different wing, radar and avionics to meet the Indian Air Force air superiority doctrine requirements. Hindustan Aeronautics Limited (HAL) will be responsible for the development of the Indian version while Sukhoi/UAC will take responsibility for the Russian fighter. The Russian fifth generation fighter primary role will be air-to-air engagements with secondary ground/surface attack capabilities. The PAK FA T-50 prototype carried out its maiden flight on January 29, 2010, with an intended entry into service date by 2016 or 2017. About 300 fifth generation fighters would be produced for the Russian Air Force between 2015 and 2025. Final specifications remain uncertain, but Russians hope to match US Air Force F/A-22 Raptor and F-35 capabilities while outperforming Typhoon, Rafale and Gripen multi-role fighters. As of 2014, it seems that the PAK FA T-50 will outperform all of them by far in the air-to-air role. According to Sukhoi the fifth-generation fighter will feature high maneuverability, stealth and supersonic cruise speed with the ability to use guided-precision air-to-surface weapons to destroy ground- and sea-based targets. The assembly line will be located at Komsomolsk-on-Amur aircraft-manufacturing plant in Russia's Far East.

Air & Air Defense Specifications
Crew 1
Max Speed 2600.0 km/h
Range 3500.0 km
Service Ceiling 20000 m
Wingspan 14.80 m
Overview (Deagel)
Group Multi-Role Fighters
Status Active
Also Known As Frazor, PAK FA, Su-50
Origin Russia
Contractors UAC*, NAPO, Sukhoi
Initial Operational Capability (IOC) 2016
First Flight January 29, 2010
Total Production 13
Development Cost USD $20.0 billion
Unitary Cost USD $30 million
Specifications (Deagel)
Crew 1
Internal Stations 10
Number of Engines 2
Area — Radar Cross Section (RCS) 0.10 square meter
Area — Wing Area 78.8 square meter
Dimensions — Height 5.5 meter
Dimensions — Length 22 meter
Dimensions — Main Gun Caliber 30 millimeter
Dimensions — Wingspan 14.8 meter
G-load — Max Maneuvering Load Factor 9 g
Mass — Max Takeoff Thrust 64,000 pound
Mass — Max Takeoff Weight 35,480 kilogram
Mass — Payload 10,000 kilogram
Performance — Ceiling 20,000 meter
Performance — Ferry Range with One In-Flight Refueling 5,500 kilometer
Performance — Max Range 3,500 kilometer
Performance — Radius of Operation 1,750 kilometer
Performance — Take Off Run Distance 300 meter
Speed — Cruise Speed 0.90 mach
Speed — Supercruise Speed 1.3 mach
Speed — Top Speed at High Altitude 2,600 kph
Time — Flight Endurance 3.3 hour
Gear (Deagel)
Item 1 Air-to-Air Missiles: R-37M
Item 2 Air-to-Air Missiles: R-77M (6)
Item 3 Air-to-Air Missiles: RVV-MD
Item 4 Air-to-Air Missiles: RVV-SD
Item 5 Anti-Radiation Missiles: Kh-31PD
Item 6 Anti-Radiation Missiles: Kh-58UShKA
Item 7 Anti-Ship Missiles: Kh-35UE
Item 8 Bombs: Drel (6)
Item 9 Bombs: KAB-250LG-E (6)
Item 10 Bombs: KAB-250S-E (6)
Item 11 ESM & Warning Systems: 101KS-U (1)
Item 12 Fighter Aircraft Engines: AL-41F1 (2)
Item 13 Jamming Systems: 101KS-O (1)
Item 14 Jamming Systems: Himalayas (1)
Item 15 Medium Caliber Cannons: GSh-301 (1)
Item 16 Optronic Systems: 101KS-N (1)
Item 17 Optronic Systems: OLS-50M (1)
Item 18 Radar Systems: Byelka (1)
Item 19 Standoff Weapons: Kh-38MAE
Item 20 Standoff Weapons: Kh-38MKE
Item 21 Standoff Weapons: Kh-38MLE
Item 22 Standoff Weapons: Kh-38MTE
Variants
Variant 1 T-50
Variant 2 FGFA
Variant 3 Su-57
Variant 4 Su-57E
Variant 5 Su-57D
Variant 6 Su-57M
Variant 7 Su-57K
Details
Country of Origin Russia
Category Multirole Aircraft
Air > Multirole Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
22 m
Width
14.8 m
Height
5.5 m
Weight
35480 kg
Operators (2)
Russia
India
Something went wrong. Please reload the page. Reload