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Comparison of Lockheed Martin F-22 Raptor and Sukhoi Su-57 (T-50 / PAK FA)


Direct side-by-side comparison of two aircraft.


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Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database.

Notes: Some entries contain '0', 'not available', or an 'NA' value. This is more common with conceptual, experimental, and x-plane designs. Rotary-wing system (i.e. helicopters) values include main rotor diameter as part of width/wingspan measurement. UAV entries may display crew values as '0', not taking into account ground-based controllers.

SUBJECTS
Lockheed Martin F-22A Raptor
5th Generation Air Dominance Fighter
Sukhoi T-50 / PAK FA
5th Generation Multi-Role Stealth Aircraft
BASICS
CREW
1
CREW
1
PRODUCTION
195 units [Diff.+185]
PRODUCTION
10 units [Diff.-185]
DIMENSIONS
LENGTH
62.07 ft (18.92 m) [Diff.-10.10 ft]
LENGTH
72.18 ft (22.00 m) [Diff.+10.10 ft]
WIDTH/SPAN
44.49 ft (13.56 m) [Diff.-2.10 ft]
WIDTH/SPAN
46.59 ft (14.20 m) [Diff.+2.10 ft]
HEIGHT
16.47 ft (5.02 m) [Diff.-3.38 ft]
HEIGHT
19.85 ft (6.05 m) [Diff.+3.38 ft]
SIZE COMPARISON
NOTES: Shapes below depict aircraft from wingtip-to-wingtip / nose-to-tail assuming aircraft are being viewed from overhead perspective (the nose pointing towards the top of the screen). Helicopter widths include main rotor diameter. If any dimensional values are "NA" in the database then the presented shapes may appear skewed.
Compare aircraft size graphic
Lockheed Martin F-22A Raptor
Compare aircraft size graphic
Sukhoi T-50 / PAK FA
WEIGHTS
EMPTY WT
31,998 lb (14,514 kg) [Diff.-8,788 lb]
EMPTY WT
40,786 lb (18,500 kg) [Diff.+8,788 lb]
MTOW
54,999 lb (24,947 kg) [Diff.-26,572 lb]
MTOW
81,571 lb (37,000 kg) [Diff.+26,572 lb]
INSTALLED POWER
2 x Pratt & Whitney F119-PW-100 afterburning turbofans developing 35,000 lb of thrust each.
2 x NPO Saturn / FNPTS MMPP Salyut AL-41F1 turbofan engines developing 35,000 lb of thrust each (T-50 prototype).
PERFORMANCE
SPEED
1,599 mph (2,574 kph) [Diff.-16 mph]
SPEED
1,616 mph (2,600 kph) [Diff.+16 mph]
RANGE
2,000 miles (3,218 km) [Diff.-1,107 miles]
RANGE
3,107 miles (5,000 km) [Diff.+1,107 miles]
CEILING
50,000 ft (15,240 m) [Diff.-15,617 feet]
CEILING
65,617 ft (20,000 m) [Diff.+15,617 feet]
ARMAMENT
STANDARD:
1 x 20mm internal automatic cannon.

AIR-TO-AIR, STEALTH:
2 x AIM-9 Sidewinders short-ranged air-to-air missiles (internal side weapons bays).
6 x AIM-120 AMRAAM medium-ranged air-to-air missiles (Internal ventral weapons bay).

AIR-TO-AIR, NON-STEALTH:
4 x AIM-9 Sidewinder short-ranged, air-to-air missiles (External, underwing, outboard).
2 x AIM-9 Sidewinder short-ranged air-to-air missiles (Internal side weapons bays).
6 x AIM-120 AMRAAM medium-ranged, air-to-air missiles (Internal ventral weapons bay).

AIR-TO-GROUND, STEALTH:
2 x AIM-9 Sidewinder short-ranged air-to-air missiles (Internal side weapons bays).
2 x AIM-120 AMRAAM medium-ranged, air-to-air missiles (Internal ventral weapons bay).
2 x 1,000lb GBU-32 Joint Direct Munitions (JDAM) (Internal ventral weapons bay).

OPTIONAL, AIR-TO-GROUND, STEALTH:
8 x 250lb GBU-39 Small Diameter Bombs (SDBs) (Internal ventral weapons bay) in place of JDAM.

Air-Launched Cruise Missiles (ALCMs) also supported.

OPTIONAL, MISCELLANEOUS:
2 x 600 US Gallon external fuel drop tanks underwing, inboard.
STANDARD:
1 OR 2 x 30mm GSh-30-1 internal cannon(s).

OPTIONAL:
Air-to-air and air-to-surface missiles; guided bombs across internal (two or four internal bays) and up to six external hardpoints.
GOING FURTHER
View Entry
(Lockheed Martin F-22 Raptor)
View Entry
(Sukhoi Su-57 (T-50 / PAK FA))

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