2 × fixed, forward-firing 7.62 mm ShKAS machine guns in
forward fuselage, 2 × fixed, forward-firing 20 mm ShVAK
cannons in wing roots, 6 × fixed, forward-firing 7.62 mm
ShKAS machine guns in in trays under wings
Built
92 units
Polikarpov I-15, 1933
Length
6.10 m (20 ft)
Wingspan
9.75 m (32 ft)
Height
2.20 m (7 ft 3 in)
Wing area
23.55 m² (236 ft²)
Empty weight
1,012 kg (2,231 lb)
Loaded weight
1,415 kg (3,120 lb)
Powerplant
1× M-22 radial engine, 353 kW (473 hp)
Maximum speed
350 km/h (220 mph)
Range
500 km (310 mi)
Service ceiling
7,250 m (23,800 ft)
Rate of climb
7.6 m/s (1,490 ft/min)
Wing loading
65 kg/m² (13 lb/ft²)
Power/mass
0.25 kW/kg (0.15 hp/lb)
Armament
4 × fixed forward-firing 7.62 mm PV-1 machine guns or 2
× fixed forward-firing 12.7 mm BS machine guns
Bombs
100 kg (220 lb)
Rockets
6 × RS-82
Built
614
units
Polikarpov I-15bis, 1934
Length
6.28 m (20 ft)
Wingspan
10.20 m (32 ft)
Height
2.20 m (7 ft 3 in)
Wing area
22.5 m² (242 ft²)
Empty weight
1,310 kg (2,885 lb)
Loaded weight
1,730 kg (3,810 lb)
Powerplant
1× M-25 radial engine, 750 hp
Maximum speed
379 km/h (237 mph)
Range
770 km (481 mi)
Service ceiling
9,800 m (32,150 ft)
Rate of climb
10.4 m/s (2.050 ft/min)
Wing loading
77 kg/m² (15.75 lb/ft²)
Armament
4 × fixed forward-firing 7.62 mm PV-1 machine guns
2 × fixed forward-firing 7.62 mm (0.30 in) ShKAS machine
guns in upper cowling, 2 × fixed forward-firing 20 mm
(0.79 in) ShVAK cannons in the wings, 6 × unguided RS-82
rockets or up to 500 kg (1,102 lb) of bombs
Mikoyan-Gurevich MiG-1, 1940
Length
8.16 m (26 ft 9 in)
Wingspan
10.20 m (33 ft 5 in)
Height
2.62 m (8 ft 7 in)
Wing area
17.5 m² (188 ft²)
Airfoil
Clark YH
Empty weight
2,602 kg (5,736 lb)
Loaded weight
3,099 kg (6,832 lb)
Max takeoff weight
3,319 kg (7,317 lb)
Powerplant
1× Mikulin AM-35A liquid-cooled V-12, 350
hp
Maximum speed
657 km/h (410 mph)
Range
580 km (362 mi)
Service ceiling
12,000 m (39,370 ft)
Rate of climb
16.8 m/s (3,306 ft/min)
Wing loading
177 kg/m² (36 lb/ft²)
Power/mass
0.32 kW/kg (0.20 hp/lb)
Armament
1 × 12.7 mm BS machine gun, 2 × 7.62 mm ShKAS machine
guns
640 km/h (398 mph, 346 knots) at 7,800 m (25,600 ft)
Maximum speed at sea level
505 km/h (314 mph, 273 knots)
Combat range
820 km (510 mi,443 NM)
Service ceiling
12,000 m (39,400 ft)
Wing loading
155 kg/m² (39.3 lb/ft²)
Power/mass
0.30 kW/kg (0.18 hp/lb)
Climb to 8,000 m (26,250 ft)
10.28 min
Armament
1 × 12.7 mm UBS machine gun, 2 × 7.62 mm ShKAS machine
guns, 2 × 100 kg (220 lb) bombs, 2 spray containers for
chemicals, gas or flammable liquids or 6 × 82 mm RS-82
rockets
1 × 20 mm ShVAK cannon in the nose, 2 × 12.7 mm UBK
machine guns in the fuselage, 1 × 12.7 mm UBT machine
gun in dorsal turreб
t1 × 7.62 mm ShKAS machine gun in tail
1 × 20 mm (0.8 in) ShVAK cannon, 1 × 12.7 mm (0.5 in)
Berezin UBS machine gun. One-second salvo weight of fire
2 kg (4.4 lb) with both the cannon and the machine gun
using high-explosive ammunition.
1 × 37 mm Nudelman N-37 cannon with 30 rounds (1 × 45
mm Nudelman N-45 could be fitted instead), 2 × 23 mm
Nudelman-Suranov NS-23 cannon with 200 rpg
Bombs
Up to 500 kg (1,102 lb) of bombs (1 × FAB-500 or 2 ×
FAB-250)
Lavochkin La-9 Fritz, 1946
Length
8.63 m (28 ft 4 in)
Wingspan
9.80 m (32 ft 2 in)
Height
3.56 m (11 ft 8 in)
Wing area
17.6 m² (189 ft²)
Empty weight
2,638 kg (5,816 lb)
Loaded weight
3,425 kg (7,551 lb)
Max takeoff weight
3,676 kg (8,104 lb)
Powerplant
1× Shvetsov ASh-82FN air-cooled radial engine with a
two-stage supercharger and fuel injection, 1,380 kW
(1,850 hp)
Maximum speed
690 km/h (428 mph) at altitude
Range
1,735 km (1,077 mi)
Service ceiling
10,800 m (35,433 ft)
Rate of climb
17.7 m/s (3,484 ft/min)
Wing loading
195 kg/m² (40 lb/ft²)
Power/mass
0.40 kW/kg (0.25 hp/lb)
Armament
4 × 23 mm Nudelman-Suranov NS-23 cannons, 75 rpg
Built
1882 units
Lavochkin La-11, 1947
Length
8.62 m (28 ft 3 in)
Wingspan
9.80 m (32 ft 2 in)
Height
3.47 m (11 ft 5 in)
Wing area
17.6 m² (189 ft²)
Empty weight
2,770 kg (6,107 lb)
Loaded weight
3,730 kg (8,223 lb)
Max takeoff weight
3,996 kg (8,810 lb)
Powerplant
1× Shvetsov ASh-82FN air-cooled radial engine with a
two-stage supercharger and fuel injection, 1,380 kW
(1,850 hp)
Maximum speed
674 km/h (419 mph) at altitude
Range
2,235 km (1,388 mi)
Service ceiling
10,250 m (33,628 ft)
Rate of climb
758 m/min (2,487 ft/min)
Wing loading
212 kg/m² (44 lb/ft²)
Power/mass
0.37 kW/kg (0.23 hp/lb)
Armament
3 × 23 mm Nudelman-Suranov NS-23 cannons, 75 rounds per
gun
Built
1182 units
Yakovlev Yak-17 Feather, 1948
Length
8.70 m (28 ft 6 in)
Wingspan
9.20 m (30 ft 2 in)
Height
2.30 m (7 ft 7 in)
Wing area
14.9 m² (160 ft²)
Empty weight
2,081 kg (4,578 lb)
Loaded weight
2,890 kg (6,358 lb)
Max takeoff weight
3,240 kg (7,128 lb)
Powerplant
1× Klimov RD-10A turbojet, 8.9 kN (2,000 lbf)
Maximum speed
748 km/h (468 mph)
Range
395 km (247 miles)
Service ceiling
12,750 m (41,820 ft)
Rate of climb
12 m/s (2362 ft/min)
Wing loading
194 kg/m² (40 lb/ft²)
Thrust/weight
0.31
Armament
2x 23 mm Nudelman-Suranov NS-23 aircraft cannons with
60 rounds per barrel
Built
430 units
Lavochkin La-15 Fantail, 1949
Length
9.56 m (31 ft 4 in)
Wingspan
8.83 m (29 ft 0 in)
Height
3.8 m (12 ft 5-39/64 in)
Wing area
16.167 m² (173.83 ft²)
Empty weight
3000 kg (6,500lb)
Loaded weight
3,800 kg (8,490 lb)
Powerplant
1× Klimov RD-500 turbojet, 15.6 kN (3,495 lbf)
Maximum speed
1,026 km/h (554 kn, 638 mph)
Range
1,170 km (632 nmi, 730 mi)
Service ceiling
13,500 m (44,290 ft)
Rate of climb
31.7 m/s (6,240 ft/min)
Wing loading
238 kg/m² (48.7 lb/ft²)
Armament
3 × 23 mm Nudelman-Suranov NS-23 cannon
Built
235 units
Yakovlev Yak-23 Flora, 1949
Length
8.12 m (26 ft 8 in)
Wingspan
8.73 m (28 ft 8 in)
Height
3.31 m (10 ft 10 in)
Wing area
13.50 m² (145 ft²)
Empty weight
1,980 kg (4,356 lb)
Loaded weight
3,384 kg (7,445 lb)
Max takeoff weight
kg (lb)
Powerplant
1× Klimov RD-500 turbojet, 15.6 kN (3,500 lbf)
Maximum speed
923 km/h (577 mph)
Range
1,400 km (875 mi)
Service ceiling
14,800 m (48,500 ft)
Rate of climb
41.4 m/s (8150 ft/min)
Wing loading
251 kg/m² (51 lb/ft²)
Thrust/weight
0.46
Armament
2 × 23 mm Nudelman-Rikhter NR-23 with 90 rpg
Built
310 units
Mikoyan-Gurevich MiG-15 Fagot, 1947
Length
10.11 m (33 ft 2 in)
Wingspan
10.08 m (33 ft 1 in)
Height
3.70 m (12 ft 2 in)
Wing area
20.6 m² (221.74 ft²)
Airfoil
TsAGI S-10 / TsAGI SR-3
Empty weight
3,580 kg (7,900 lb)
Loaded weight
4,960 kg (10,935 lb)
Max takeoff weight
6,105 kg (13,460 lb)
Fuel capacity
1,400 L (364 US gal))
Powerplant
1× Klimov VK-1 turbojet, 26.5 kN (5,950 lbf)
Maximum speed
1,075 km/h (668 mph)
Cruise speed
840 km/h (520 mph)
Range
1,200 km, 1,975 km with external tanks (745 mi / 1,225
mi)
Service ceiling
15,500 m (50,850 ft)
Rate of climb
50 m/s (9,840 ft/min)
Wing loading
240.8 kg/m² (49.3 lb/ft²)
Thrust/weight
0.54
Armament
2x NR-23 23mm cannons in lower left fuselage (80 rounds
per gun, 160 rounds total),1x Nudelman N-37 37 mm cannon
in lower right fuselage (40 rounds total),2x 100 kg (220
lb) bombs, drop tanks, or unguided rockets on 2
underwing hardpoints.
1 x Tumansky
R-28 V-300 turbojet, 66.7 kN (15,000 lbf)
Powerplant
2× Rybinsk
RD-38 turbojets, 31.9 kN (7,870 lbf>) each
Maximum speed
1 280 km/h (795
mph)
Range
1,300 km (807
miles)
Service ceiling
11,000 m
(36,089 ft)
Rate of climb
4,500 m/min
(14,760 ft/min)
Wing loading
476 kg/m²
Armament
Guns
GSh-23L 23mm
gun pod (GP-9). This gun could be carried in one or two
PUK-23-250 pods fixed under the external pylons of
wings.
Bombs
two FAB-500 or
four FAB-250 under pylons, two incendiary ZB-500, or two
nuclear tactical RN-28.
Missiles
two anti-ship
or air-to-surface Kh-23. Each missile weighed 285 kg,
was radiocontrolled and had 10 kilometres of range. The
Kh-23 requires a guidance pod on one of the pylons. R-60
or R-60M air-to-air missiles could be carried under the
external pylons.
1,430 km (772
nmi, 888 mi) with maximum internal fuel
Ferry range
2,100 km (1,800
mi) with 1 drop tank
Service ceiling
18,013 m
(59,100 ft)
Rate of climb
initial 330 m/s
average 109 m/s 0-6000 m (65,000 ft/min)
Wing loading
442 kg/m² (90.5
lb/ft²)
Thrust/weight
1.01
Armament
1 x 30 mm
GSh-30-1 cannon with 150 rounds.7 Hard points 6 × pylons
under-wing, 1 x under fuselage. Up to 3,500 kg (7,720
lb) of weapons including six air-to-air missiles — a mix
of semi-active radar homing (SARH) and AA-8 "Aphid",
AA-10 "Alamo", AA-11 "Archer", AA-12 "Adder", FAB
500-M62, FAB-1000, TN-100, ECM Pods, S-24, AS-12, AS-14
Sukhoi Su-27 Flanker, 1977
Length
21.9 m (72 ft)
Wingspan
14.7 m (48 ft 3
in)
Height
5.92 m (19 ft 6
in)
Wing area
62 m² (667 ft²)
Empty weight
16,380 kg
(36,100 lb)
Loaded weight
23,430 kg
(51,650 lb)
Max takeoff
weight
30,450 kg
(67,100 lb)
Powerplant
2× Saturn/Lyulka
AL-31F turbofans
Dry thrust
7,670 kgf
(75.22 kN, 16,910 lbf) each
Thrust with
afterburner
12,500 kgf
(122.6 kN, 27,560 lbf) each
Leading edge
sweep
42°
Maximum speed
Mach 2.35
(2,500 km/h, 1,550 mph) at altitude
Range
3,530 km (2,070
mi) at altitude; (1,340 km / 800 mi at sea level)
Service ceiling
18,500 m
(62,523 ft)
Rate of climb
300 m/s
(54,000 ft/min)
Wing loading
371 kg/m² (76
lb/ft²)
Thrust/weight
1.09
Armament
1 × 30 mm
GSh-30-1 cannon with 150 rounds, 8,000 kg (17,600 lb) on
10 external pylons, Up to 6 × medium-range AA missiles
R-27, 2 × short-range heat-seeking AA missiles R-73
Mikoyan-Gurevich MiG-31 Foxhound, 1975
Length
22.69 m (74 ft
5 in)
Wingspan
13.46 m (44 ft
2 in)
Height
6.15 m (20 ft 2
in)
Wing area
61.6 m² (663
ft²)
Empty weight
21,820 kg
(48,100 lb)
Loaded weight
41,000 kg
(90,400 lb)
Max takeoff
weight
46,200 kg
(101,900 lb)
Powerplant
2× Soloviev
D-30F6 afterburning turbofans
Dry thrust
93 kN (20,900
lbf) each
Thrust with
afterburner
152 kN (34,172
lbf) each
Maximum speed
High altitude
Mach 2.83
(3,000 km/h, 1,860 mph)
Low altitude
Mach 1.2 (1,500
km/h, 930 mph)
Combat radius
720 km (450 mi)
at Mach 2.35
Ferry range
3,300 km (2,050
mi)
Service ceiling
20,600 m
(67,600 ft)
Rate of climb
208 m/s (41,000
ft/min)
Wing loading
665 kg/m² (136
lb/ft²)
Thrust/weight
0.85
Maximum g-load
5 g
Armament
1× GSh-6-23 23
mm cannon with 260 rounds. Fuselage recesses for 4× R-33
(AA-9 'Amos') or (for MiG-31M/BM only) ×6 R-37 (AA-X-13
'Arrow') long-range air-to-air missiles.Four underwing
pylons for a combination of two R-40TD1 (AA-6 'Acrid')
medium-range missiles, and 4× R-60 (AA-8 'Aphid') or 4×
R-73 (AA-11 'Archer') short-range IR missiles, or 4×
R-77 (AA-12 'Adder') medium-range missiles.
Mach 2.17
(2,300 km/h, 1,430 mph) at 10,000 m (33,000 ft) altitude
Stall speed
240 km/h (150
mp/h)
Range
3,000 km (1,860
mi)
Service ceiling
17,000 m
(55,800 ft)
Rate of climb
230m/s (45,350
ft/min)
Wing loading
483 kg/m²;
(98.9 lb/ft²)
Thrust/weight
0.83
Maximum turn
+8 g (+78 m/s²)
Landing speed
235-250 km/h
(145-155 mph)
Armament
1 × 30 mm
GSh-30-1 cannon with 150 rounds. Up to 6,500 kg (14,300
lb) of munitions on twelve external hardpoints,
including 4 R-27 and 4R-73 air-to-air missiles.
Sukhoi Su-35 Flanker-E, 1988
Length
21.9 m (72.9
ft)
Wingspan
15.3 m (50.2
ft)
Height
5.90 m (19.4
ft)
Wing area
62.0 m² (667
ft²)
Empty weight
18,400 kg
(40,570 lb)
Loaded weight
25,300 kg
(56,660 lb)
Max takeoff
weight
34,500 kg
(76,060 lb)
Powerplant
2× Saturn 117S
with TVC nozzle turbofan
Dry thrust
8,800 kgf[53]
(86.3 kN, 19,400 lbf) each
Thrust with
afterburner
14,500 kgf (142
kN, 31,900 lbf) each
Maximum speed
Mach 2.25
(2,390 km/h, 1,490 mph) at altitude
Range
3,600 km (1,940
nmi); (1,580 km, 850 nmi near ground level)
Ferry range
4,500 km (2,430
nmi) with external fuel tanks
Service ceiling
18,000 m
(59,100 ft)
Rate of climb
>280 m/s
(>55,100 ft/min)
Wing loading
408 kg/m² (84.9
lb/ft²)
Thrust/weight
1.1
Armament
1 × 30 mm GSh-30 internal cannon with 150 rounds. 2 ×
wingtip rails for R-73 (AA-11 "Archer") air-to-air
missiles or ECM pods. 12 × wing and fuselage stations
for up to 8,000 kg (17,630 lb) of ordnance, including
for a variety of ordnance including air-to-air missiles,
air-to-surface missiles, rockets, and bombs such asAA-10
Alamo R-27R, R-27ER, R-27T, R-27ET, R-27EP, R-27AE.
AA-12 Adder R-77, and the proposed R-77M1, R-77T. AA-11
Archer R-73E, R-73M, R-74M. AS-17 Krypton Kh-31A, Kh-31P
Anti-Radiation Missile. AS-20 Kh-59. AS-14 Kedge Kh-29T,
Kh-29L. KAB-500 Laser-guided bomb. KAB-1500 Laser-guided
bomb. LGB-250 laser-guided bomb. FAB-250 250kg unguided
bombs. FAB-500 500kg unguided bombs. S-25LD laser-guided
rocket, S-250 unguided rocket. B-8 unguided S-8 rocket
pods. B-13 unguided S-13 rocket pods.
Sukhoi Su-37 Flanker-F, 1996
Length
22.183 m (72 ft
9 in)
Wingspan
14.7 m (48 ft 3
in)
Height
6.43 m (21 ft 1
in)
Wing area
62.0 m² (667
ft²)
Empty weight
18,500 kg
(40,790 lb)
Max takeoff
weight
35,000 kg
(77,160 lb)
Powerplant
2× Lyulka
AL-37FU afterburning turbofans
Dry thrust
7,600 kgf (74.5
kN, 16,750 lbf) each
Thrust with
afterburner
145 kN (32,000
lbf) each
Maximum speed
Mach 2.30
(1,550 mph[9])
Range
3,700 km (2,230
mi)
Service ceiling
18,000 m
(59,100 ft)
Maximum G
loading
+9/-3 g
Armament
1 × 30 mm
GSh-30 cannon with 150 rounds, 12 × wing and fuselage
stations for up to 8,200 kg (18,080 lb) of ordnance
Mikoyan-Gurevich MiG-35 Fulcrum-F, 2007
Length
17.3 m (56 ft 9
in)
Wingspan
12 m (39 ft 4
in)
Height
4.7 m (15 ft 5
in)
Wing area
38 m2 (124 ft2)
Empty weight
11,000 kg
(24,250 lb)
Loaded weight
17,500 kg
(38,600 lb)
Max takeoff
weight
29,700 kg
(65,500 lb)
Powerplant
2× Klimov
RD-33MK afterburning turbofans
Dry thrust
5,400 kgf, 53.0
kN (11,900 lbf) each
Thrust with
afterburner
9,000 kgf, 88.3
kN (19,800 lbf) each
Maximum speed
Mach 2.25
(2,400 km/h, 1,491 mph) at altitude;1,450 km/h (901 mph)
at low-level
Range
2,000 km (1,240
mi)
Combat radius
1,000 km (620
mi)
Ferry range
3,100 km (1,930
mi) with 3 external fuel tanks
Service ceiling
17,500 m
(57,400 ft)
Rate of climb
330 m/s (65,000
ft/min)
Thrust/weight
1.14
Max Maneuvering
Load Factor
10.0 g
Guns
1× 30 mm
GSh-30-1 cannon, 150 rounds
Hardpoints
9 total (8×
under-wing, 1× centre-line)
Rockets
S-8, S-13,
S-24, S-25L, S-250 unguided and laser-guided rockets
Sukhoi T-50 PAK FA, 2010
Length
19.8 m (65.9 ft)
Wingspan
14 m (46.6 ft)
Height
6.05 m (19.8 ft)
Wing area
78.8 m ² (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, definitive version with new engine >157 kN
Fuel capability
10,300 kg (22,711 lb)
Minimum Radar Cross Section (RCS)
0.5 m²
Maximum speed
2,100 - 2,500 km/h (Mach 2+) (1,300 - 1,560 mph) ; at
17,000 m (45,000 ft) altitude
None on prototype. Apparent provision for a cannon
(most likely GSh-301).Possible two 30-mm cannons
Hardpoints
Two internal bays estimated at 4.6-4.7 metres by 1-1.1
metres. Other sources suggest two auxiliary internal
bays for short range AAMS and six external hardpoints