General characteristics
* Crew: 1
* Length: 19.8 m (65.9 ft)
* Wingspan: 14 m (46.6 ft)
* Height: 6.05 m (19.8 ft)
* Wing area: 78.8 m2 (848.1 ft2)
* Empty weight: 18,500 kg (40,785 lb)
* Loaded weight: 26,000 kg (57,320 lb)
* Useful load: 7,500 kg (combat load) (16,534 lb)
* Max takeoff weight: 37,000 kg (81,570 lb)
* Powerplant: 2× New unnamed engine by NPO Saturn and FNPTS MMPP Salyut of 175 kN each. Prototype with AL-41F1 of 147 kN each,[61] definitive version with new engine >157 kN[61]
* Maximum Fuel weight: 10,300 kg (22,711 lb)
Performance
* Maximum speed: 2,100 - 2,600 km/h (Mach 2+) (1,305 - 1,625 mph) ; at 17,000 m (45,000 ft) altitude
* Cruise speed: 1,300 - 2,100 km/h (808 - 1312.5 mph)
* Ferry range: 5,500 km (3417 miles)
* Service ceiling: 20,000 m (65,616 ft)
* Rate of climb: 350 m/sec (68,900 ft/min)
* Wing loading: 330(normal) - 470(maximum) kg/m2 (67(normal) - 96(maximum) lb/ft2)
* Thrust/weight: 1.19 at 30,000kg weight. 1.37 at 26,000kg [59]
* Maximum g-load: 10-11 g
Armament
* Guns: None on prototype. Apparent provision for a cannon (most likely GSh-301).Possible two 30mm cannons
* Hardpoints: Two internal bays estimated at 4.6-4.7 metres by 1-1.1 metres.[64] . Other sources suggest two auxiliary internal bays for short range AAMS and 6 external hardpoints
Avionics
N050(?)BRLS AFAR/AESA built by Tikhomirov NIIP and based on Tikhomirov NIIP N035 Irbis-E . It will be the second aircraft based AESA Radar to be built by Russia, the first being the Phazotron NIIR ZHUK-A Radar in the MIG-35.
Designed armament
Two Izdeliye 810 Extended beyond visual range missiles per weapons bay. Multiple Izdeliye 180 / K77M beyond visual range missiles. K74 and K30 within visual range missiles can also be carried.
Two KH38M or KH58 USHK air-to-ground missiles per weapons bay. Multiple 250–500 kg precision guided bombs per weapons bay, with a maximum of ten bombs in internal bays
Other possible loads include one 1500 kg bomb per weapons bay or two 400 km+ range anti-AWACS weapons on external hard-points. A maximum weapons load of 7500 kg is reported.
General characteristics
* Crew: 1
* Length: 62 ft 1 in (18.90 m)
* Wingspan: 44 ft 6 in (13.56 m)
* Height: 16 ft 8 in (5.08 m)
* Wing area: 840 ft² (78.04 m²)
* Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
* Empty weight: 43,430 lb (19,700 kg)
* Loaded weight: 64,460 lb (29,300 kg)
* Max takeoff weight: 83,500 lb (38,000 kg)
* Powerplant: 2× Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans
o Dry thrust: 23,500 lb[199] (104 kN) each
o Thrust with afterburner: 35,000+ lb (156+ kN) each
* Fuel capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb (11,900 kg) with two external fuel tanks
Performance
* Maximum speed:
o At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)
o Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)
* Range: >1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
* Combat radius: 410 nmi (471 mi, 759 km)
* Ferry range: 2,000 mi (1,738 nmi, 3,219 km)
* Service ceiling: 65,000 ft (19,812 m)
* Wing loading: 77 lb/ft² (375 kg/m²)
* Thrust/weight: 1.08 (1.26 with loaded weight & 50% fuel)
* Maximum design g-load: -3.0/+9.0 g
USAF poster overview of key features and armament
Armament
* Guns: 1× 20 mm (0.787 in) M61A2 Vulcan 6-barreled gatling cannon in starboard wing root, 480 rounds
* Air to air loadout:
o 6× AIM-120 AMRAAM
o 2× AIM-9 Sidewinder
* Air to ground loadout:
o 2× AIM-120 AMRAAM and
o 2× AIM-9 Sidewinder for self-protection, and one of the following:
+ 2× 1,000 lb (450 kg) JDAM or
+ 8× 250 lb (110 kg) GBU-39 Small Diameter Bombs
* Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 US gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,268 kg).
Avionics
* RWR (Radar warning receiver): 250 nmi (463 km) or more
* Radar: 125–150 miles (200–240 km) against 1 m2 (11 sq ft) targets (estimated range)[105]
* Chemring MJU-39/40 flares for protection against IR missiles.
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