Lockheed Martin F-22 Raptor vs Sukhoi Su-57 (Felon) Comparison

Aviation | Utilities | Side-by-Side Comparison

Direct side-by-side comparison of two aircraft.

Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database. 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 Su-57
5th Generation Multi-Role Stealth Aircraft

Basics

ORIGIN
United States

ORIGIN
Russia

YEAR
2005 [Diff.-14 yrs]

YEAR
2019 [Diff.+14 yrs]

CREW
1

PRODUCTION
195 units [Diff.+170]

PRODUCTION
25 units [Diff.-170]

Dimensions

LENGTH
62.1 ft (18.9 m) [Diff.-10.1 ft]

LENGTH
72.2 ft (22.0 m) [Diff.+10.1 ft]

WIDTH/SPAN
44.5 ft (13.6 m) [Diff.-2.1 ft]

WIDTH/SPAN
46.6 ft (14.2 m) [Diff.+2.1 ft]

HEIGHT
16.5 ft (5.0 m) [Diff.-3.4 ft]

HEIGHT
19.8 ft (6.1 m) [Diff.+3.4 ft]

Relative Size Comparison

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.

Lockheed Martin F-22A Raptor

Sukhoi Su-57

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]

M.T.O.W.
54,999 lb (24,947 kg) [Diff.-26,572 lb]

M.T.O.W.
81,571 lb (37,000 kg) [Diff.+26,572 lb]

Installed Power

2 x Pratt & Whitney F119-PW-100 afterburning turbofans each developing 26,000lb thrust dry and 35,000 lb of thrust with reheat.

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]

RATE-OF-CLIMB
62,000 ft/min [Diff.-2,000 feet]

RATE-OF-CLIMB
64,000 ft/min [Diff.+2,000 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.

Internal loadout rated up to 2,000lb, external mountings rated up to 5,000lb each (collectively 22,000lb of ordnance).

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 (Felon))

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