| |
|

Nieuport-11,
Anatra-Anadis,
Mosca MB bis by Bystritsky,
S-16 by Igor I. Sikorsky, Polikarpov I-1 (IL-400), Grigorovich I-2, Polikarpov I-3, Tupolev I-4, Polikarpov I-5, I-7 (Heinkel HD 37) was built by German license, Tupolev I-8. 1930, Grigorovich I-Z. 1931, Tupolev I-12 (ANT-23), Grigorovich IP-1, Polikarpov I-15, Polikarpov I-15bis, Polikarpov I-16, Kochyerigin DI-6, Polikarpov I-153, Polikarpov I-16, 1939, Mikoyan-Gurevich MiG-1, Mikoyan-Gurevich MiG-3, Petlyakov Pe-3, Yakovlev Yak-1,
Lavochkin-Gorbunov-Gudkov LaGG-3, Polikarpov I-185, Yakovlev Yak-3, Lavochkin La-5, Yakovlev Yak-7, Yakovlev Yak-9, Lavochkin La-7 Fin, Mikoyan-Gurevich MiG-9 Fargo, Yakovlev Yak-15, Sukhoi Su-9, Lavochkin La-9 Fritz, Lavochkin La-11, Yakovlev Yak-17 Feather, Lavochkin La-15 Fantail, Yakovlev Yak-23 Flora, Mikoyan-Gurevich MiG-15 Fagot, Mikoyan-Gurevich MiG-17 Fresco, Yakovlev Yak-25 Flashlight-A, Mikoyan-Gurevich MiG-19 Farmer, Yakovlev Yak-25 Flashlight-C, Sukhoi Su-9 Fishpot, Tupolev Tu-28/Tu-128 Fiddler, Mikoyan-Gurevich MiG-21 Fishbed, Yakovlev Yak-28 Firebar, Sukhoi Su-15 Flagon, Mikoyan-Gurevich MiG-23 Flogger, Mikoyan-Gurevich MiG-25 Foxbat, Yakovlev Yak-38 VTOL fighter Forger, Mikoyan-Gurevich MiG-29 Fulcrum, Sukhoi Su-27 Flanker, Mikoyan-Gurevich MiG-31 Foxhound, Sukhoi Su-30 Flanker-С, Sukhoi Su-30 Flanker-D, Sukhoi Su-35 Flanker-E, Sukhoi Su-37 Flanker-F, Mikoyan-Gurevich MiG-35 Fulcrum-F, Sukhoi T-50 PAK FA,
|
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CONTENTS:

MOSCOW:
everything about
the
Russian capital


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More→
Russian cities

Birth and death rate in Russia since 1950 till 2010.
Full list of the heads of Russia and the USSR









Советские цены на автомобили и мотоциклы в рублях и средних зарплатах

З олотые
запасы стран мира
Золотовалютные резервы стран мира
Нужен ли России золотой рубль?
Как
разбогатела Америка
Рейтинг стран мира по численности вооружённых сил
Кто и как
продавал Аляску
Почему мы
проиграли Холодную войну
Тайна
реформы 1961 года
Как
остановить вырождение нации
В
какой стране пьют больше всех?
В какой
стране больше всего убийств?
Как жил русский рабочий до революции?
|
 |
Полный
список глав Русского Государства с VIII века до наших дней. |
|
 |
Полный список глав Правительства Нашей Страны с 1802 года до
наших дней. |
|
 |
Города России
–
полный список городов с населением от 100 тысяч человек
|
|
 |
Русские,
советские и российские чины и звания и знаки их различия
|
|
 |
Зарплаты, в Российской
империи, СССР и Российской Федерации с 1897
по 2010 годы |
|
 |
Русские танки от Вездехода до Т-90
|
|
 |
Курс рубля к доллару
с 1792 по 2010 |
|
 |
Русские
автомобили с 1896 по 2010 годы |
|
 |
Русские броневики |
|
 |
Русские меры: аршин, бочка, ведро, верста, вершок,
доля, дюйм, золотник, линия, пуд, сажень, точка, фунт, чарка, шкалик,
штоф
|
|
 |
Буква ять и
её правописание |
|
 |
Русские
полки
|
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Nieuport-11, 1915
was built by French
license
|
Length |
5.8 m (19 ft 0 in) |
|
Wingspan |
7.55 m (24 ft 9 in) |
|
Height |
2.4 m (7 ft 10.5 in) |
|
Wing area |
13 m² (140 ft²) |
|
Empty weight |
344 kg (759 lb) |
|
Loaded weight |
480 kg (1,058 lb) |
|
Max takeoff weight |
550 kg (1,213 lb) |
|
Powerplant |
1× Gnome or Le Rhone 9C air-cooled rotary, 80
hp |
|
Maximum speed |
156 km/h (97 mph) |
|
Range |
330 km (205 miles) |
|
Service ceiling |
4,600 m (15,090 ft) |
|
Rate of climb |
15 mins to 3,000 m (9,840 ft) |
|
Power/mass |
1.49 kW/kg (0.09 hp/lb) |
|
Armament |
1 × Hotchkiss or Lewis machine gun |
|
|

Anatra-Anadis, 1916
|
Length |
7.75
m |
|
Wingspan |
11.40
m |
|
Wing area |
37 m2 |
|
Empty weight |
665
kg |
|
Max takeoff weight |
1165
kg. |
|
Powerplant |
Hispano-Suiza,
150 hp |
|
Maximum speed |
153
km/h |
|
Service ceiling |
|
|
Rate of climb |
133 m/min |
|
Armament |
2×7.7
Lewis |
|
|

Mosca MB bis by Bystritsky,1916
|
Length |
6.1 m |
|
Wingspan |
7.2 m |
|
Wing area |
12.1 m2 |
|
Empty weight |
487
kg |
|
Max takeoff weight |
1165
kg. |
|
Powerplant |
Le
Rhone 9C air-cooled rotary, 59.6 kW (80 hp) |
|
Maximum speed |
130
km/h |
|
Service ceiling |
3200 m |
|
Rate of climb |
133 m/min |
|
Armament |
2×7.7
Lewis |
|
|

S-16
by Igor I. Sikorsky, 1916
|
Length |
5.9 m |
|
Wingspan |
8 m |
|
Wing area |
25.3 m2 |
|
Empty weight |
407
kg |
|
Max takeoff weight |
1165
kg. |
|
Powerplant |
Le
Rhone 9C air-cooled rotary, 59.6 kW (80 hp) |
|
Maximum speed |
125
km/h |
|
Service ceiling |
3500 m |
|
Armament |
1×7.7
Vickers |
|
|

Polikarpov I-1 (IL-400), 1923
|
Length |
5.9 m |
|
Wingspan |
10.8 m |
|
Wing area |
25.3 m2 |
|
Empty weight |
112
kg |
|
Max takeoff weight |
1165
kg. |
|
Powerplant |
1×
Liberty water-cooled 45-degree V12 engine, 298 kW (400
hp) |
|
Maximum speed |
260 km/h |
|
Service ceiling |
5500 m |
|
Armament |
2×7.62
PV |
|
Built |
33 units |
|
|

Grigorovich I-2, 1924
|
Length |
7.32 m (24 ft 0 in) |
|
Wingspan |
10.80 m (35 ft 5 in) |
|
Height |
3.00 m (9 ft 10 in) |
|
Wing area |
23.4 m² (252 ft²) |
|
Empty weight |
1,152 kg (2,540 lb) |
|
Loaded weight |
1,575 kg (3,472 lb) |
|
Powerplant |
1× M-5 water-cooled 45-degree V12 engine, 400
hp |
|
Maximum speed |
235 km/h (147 mph) |
|
Range |
600 km (374 miles) |
|
Service ceiling |
5,340 m (17,515 ft) |
|
Rate of climb |
420 m/min (1,377 ft/min) |
|
Wing loading |
67 kg/m² (14 lb/ft²) |
|
Power/mass |
0.19 kW/kg (0.12 hp/lb) |
|
Armament |
2 × 7.62 mm PV-1 machine guns |
|
Built |
211 units |
|
|

Polikarpov I-3, 1928
|
Length |
8.08 m (26 ft 6 in) |
|
Wingspan |
11 m (36 ft 1 in) |
|
Wing area |
27.85 m² (299.8 ft²) |
|
Airfoil |
Clark Y |
|
Empty weight |
1,400 kg (3,086 lb) |
|
Loaded weight |
1,846 kg (4,070 lb) |
|
Powerplant |
1× BMW VI V12 engine, 545 kW (730 hp) |
|
Maximum speed |
278 km/h (150 kn, 173 mph) |
|
Range |
585 km (316 nmi, 364 mi) |
|
Service ceiling |
7,200 m (23,620 ft) |
|
Wing loading |
66 kg/m² (14 lb/ft²) |
|
Power/mass |
295 W/kg (0.18 hp/lb) |
|
Time to altitude |
12.6 min to 5,000 m (16,400 ft) |
|
Horizontal turn time |
14 sec |
|
Armament |
2 × 7.62 mm (0.3 in) PV-1 machine gun |
|
Built |
399 units |
|
|

Tupolev I-4, 1927
|
Length |
7.27 m (23 ft 10 in) |
|
Wingspan |
11.42 m (37 ft 5 in) |
|
Height |
2.82 m (9 ft 2 in) |
|
Wing area |
23.8 m² (256 ft²) |
|
Empty weight |
978 kg (2,156 lb) |
|
Loaded weight |
1,430 kg (3,153 lb) |
|
Powerplant |
1× M-22 piston radial Bristol Jupiter , 460
hp |
|
Maximum speed |
257 km/h (160 mph) |
|
Range |
840 km (524 mi) |
|
Service ceiling |
7,655 m (25,100 ft) |
|
Rate of climb |
555 m/min (1,820 ft/min) |
|
Wing loading |
60 kg/m² (12 lb/ft²) |
|
Power/mass |
0.25 kW/kg (0.15 hp/lb) |
|
Armament |
2 × 7.62 mm PV-1 machine guns |
|
Built |
369
units |
|
|

Polikarpov I-5, 1931
|
Length |
6.78 m (22 ft 3 in) |
|
Upper wingspan |
10.24 m (33 ft 7 in) |
|
Lower wingspan |
7.4 m (24 ft 3 in) |
|
Wing area |
21.3 m2 (229 sq ft) |
|
Airfoil |
Göttingen-436 |
|
Empty weight |
934 kg (2,059 lb) |
|
Gross weight |
1,355 kg (2,987 lb) |
|
Fuel capacity |
165 |
|
Powerplant |
1 × Shvetsov M-22 9-cylinder, single-row radial engine,
358 kW (480 hp) |
|
Propellers |
2-bladed duralumin, 2.7 m (8 ft 10 in) diameter |
|
Maximum speed |
278 km/h (173 mph; 150 kn) at sea level |
|
Range |
660 km (410 mi; 356 nmi) |
|
Service ceiling |
7,500 m (24,606 ft) |
|
Time to altitude |
1.6 minutes to 1,000 metres (3,300 ft) |
|
Horizontal turn time |
10 sec |
|
Guns |
2 × 7.62-mm PV-1 machine guns |
|
Bombs |
2 × 22-lb (10-kg) |
|
Built |
809 units |
|
|

I-7 (Heinkel HD 37), 1931
was built by
German license
|
Length |
6.95 m (22 ft 10 in) |
|
Wingspan |
10.00 m (32 ft 10 in) |
|
Height |
3.20 m (10 ft 6 in) |
|
Wing area |
25.9 m² (279 ft²) |
|
Empty weight |
1,419 kg (3,121 lb) |
|
Gross weight |
1,792 kg (3,942 lb) |
|
Powerplant |
1 × Mikulin M-17F, 540 kW (730 hp) |
|
Maximum speed |
291 km/h (182 mph) |
|
Range |
700 km (440 miles) |
|
Service ceiling |
7,200 m (23,600 ft) |
|
Rate of climb |
9.7 m/s (1,900 ft/min) |
|
Armament |
2 × fixed, forward-firing 7.62 mm (.30 in) PV-1 machine
guns |
|
Built |
131 unuts |
|
|

Tupolev I-8, 1930
|
Length |
6.70 m (21 ft 11¾ in) |
|
Wingspan |
9 m (29 ft 6 in) |
|
Wing area |
20 m² (215.3 ft²) |
|
Empty weight |
1,000 kg (2,205 lb) |
|
Loaded weight |
1,424 kg (3,139 lb) |
|
Powerplant |
1× Curtiss V-1570 V-12 piston engine, 625 hp |
|
Maximum speed |
310 km/h (167 kn, 193 mph) at 3,000 m (9,845 m) |
|
Range |
440 km (238 nmi, 273 mi) |
|
Service ceiling |
8,500 m (27,887 ft) |
|
Wing loading |
71 kg/m² (15 lb/ft²) |
|
Power/mass |
327 W/kg (0.2 hp/lb) |
|
Time to altitude |
6 min to 5,000 m (16,405 ft) |
|
Armament |
2 × 7.62 mm (0.3 in) PV-1 machine guns |
|
|

Grigorovich I-Z. 1931
|
Length |
7.65 m (25 ft 1 in) |
|
Wingspan |
11.5 m (37 ft 9 in) |
|
Wing area |
19.5 m² (209.9 ft²) |
|
Empty weight |
1,180 kg (2,601 lb) |
|
Loaded weight |
1,648 kg (3,633 lb) |
|
Powerplant |
1× M-22 radial engine, 358 kW (480 hp) |
|
Maximum speed |
259 km/h (140 knots, 161 mph) |
|
Range |
600 km (324 nm, 373 mi) |
|
Service ceiling |
7,000 m (23,000 ft) |
|
Wing loading |
85 kg/m² (17 lb/ft²) |
|
Power/mass |
217 W/kg (0.13 hp/lb) |
|
Time to altitude |
14 min to 5,000 m (16,400 ft) |
|
Horizontal turn time |
17 sec |
|
Armament |
1×7.62 mm (0.3 in) PV-1 machine gun, 2×76.2 mm (3 in)
Kurchevski DRP (APK) cannon |
|
Built |
71 units |
|
|

Tupolev I-12 (ANT-23), 1931 |
|
Length |
9.5 m (31 ft 2 in) |
|
Wingspan |
15.6 m (51 ft 2 in) |
|
Wing area |
30 m² (322.9 ft²) |
|
Loaded weight |
2,400 kg (5,291 lb) |
|
Powerplant |
2× Gnome-Rhône 9K Jupiter-6 radial engines, 392 kW (525
hp) each |
|
Maximum speed |
300 km/h (162 kn, 186 mph) |
|
Wing loading |
80 kg/m² (16 lb/ft²) |
|
Power/mass |
326 W/kg (0.2 hp/lb) |
|
Armament |
2×76.2 mm (3 in) APK recoilless rifles |
|
|

Grigorovich IP-1, 1935
|
Weight |
7.23 m (23 ft 9 in) |
|
Wingspan |
10.97 m (36 ft 0 in) |
|
Wing area |
20.0 m² (215 ft²) |
|
Empty weight |
1,200 kg (2,646 lb) |
|
Gross weight |
1,880 kg (4,145 lb) |
|
Powerplant |
1 × Shvetsov M-25, 530 kW (710 hp) |
|
Maximum speed |
410 km/h (255 mph) |
|
Range |
600 km (373 miles) |
|
Service ceiling |
8,300 m (27,230 ft) |
|
Rate of climb |
12.8 m/s (2,520 ft/min) |
|
Armament |
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 |
|
Bombs |
150 kg (330 lb) |
|
Rockets |
6 × RS-82 |
|
Built |
2408
units |
|
|

Polikarpov I-16, Type 1, 1933
|
Length |
5.86 m (19 ft 3 in) |
|
Wingspan |
9 m (29 ft 6 in) |
|
Height |
3.25 m (10 ft 8 in) |
|
Wing area |
14.5 m² (156.1 ft²) |
|
Empty weight |
1,490 kg (3,285 lb) |
|
Loaded weight |
1,941 kg (4,279 lb) |
|
Max takeoff weight |
2,095 kg (4,619 lb) |
|
Powerplant |
1× Shvetsov M-22 supercharged air-cooled radial engine,
480 hp, driving a two-blade propeller |
|
Maximum speed |
362 km/h (226 mph) at 3,000 m (9,845 ft) |
|
Service ceiling |
9,700 m (31,825 ft) |
|
Rate of climb |
11.4 m/s (2,244 ft/min) |
|
Wing loading |
134 kg/m² (27 lb/ft²) |
|
Armament |
2 × fixed forward-firing 7.62 mm (0.30 in)
unsynchronized ShKAS machine guns in the wings with 900
rpg. |
|
|

Kochyerigin DI-6, 1934
|
Crew |
2 |
|
Length |
6.87 m (22 ft 6 in) |
|
Wingspan |
9.94 m (32 ft 7 in) |
|
Height |
3.2 m (10 ft 6 in) |
|
Wing area |
25.15 m² (270.7 ft²) |
|
Empty weight |
1,360 kg (2,998 lb) |
|
Loaded weight |
1,955 kg (4,310 lb) |
|
Powerplant |
1× Shvetsov M-25 radial engine, 522 kW (700 hp) |
|
Maximum speed |
372 km/h (201 knots, 231 mph) |
|
Range |
500 km (270 nm, 311 mi) |
|
Service ceiling |
7,700 m (25,262 ft) |
|
Wing loading |
78 kg/m² (16 lb/ft²) |
|
Power/mass |
267 W/kg (0.16 hp/lb) |
|
Time to altitude |
10 min to 5,000 m (16,400 ft) |
|
Horizontal turn time |
12 sec |
|
Armament |
3× 7.62 mm (0.3 in) ShKAS machine guns, two
unsynchronized firing forward and one on a rear-facing
mount, 750 rounds per a gun |
|
Bombs |
40 kg (88 lb) |
|
Built |
222 units |
|
|

Polikarpov I-153, 1938
|
Length |
6.18 m (20 ft 3 in) |
|
Wingspan |
|
Top wing |
10.0 m (32 ft 10 in) |
|
Bottom wing |
7.5 m (24 ft 7 in) |
|
Height |
3.0 m (9 ft 10 in) |
|
Wing area |
22.1 m² (237.8 ft²) |
|
Empty weight |
1,348 kg (2,972 lb) |
|
Loaded weight |
1,765 kg (3,891 lb) |
|
Max takeoff weight |
1,859 kg (4,098 lb) |
|
Powerplant |
1× Shvetsov M-62 radial engine, 597 kW (800 hp) |
|
Maximum speed |
426 km/h (265 mph) |
|
Range |
740 km (460 mi) |
|
Service ceiling |
11,000 m (36,089 ft) |
|
Rate of climb |
15 m/s (2,985 ft/min) |
|
Wing loading |
80 kg/m² (16 lb/ft²) |
|
Power/mass |
0.34 kW/kg (0.21 hp/lb) |
|
Armament |
4 × 7.62 mm ShKAS machine guns, 2,500 rounds of
ammunition total |
|
Built |
3,437 |
|
|

Polikarpov I-16, Type 24, 1939
|
Length |
6.13 m (20 ft 1 in) |
|
Wingspan |
9 m (29 ft 6 in) |
|
Height |
3.25 m (10 ft 8 in) |
|
Wing area |
14.5 m² (156.1 ft²) |
|
Empty weight |
1,490 kg (3,285 lb) |
|
Loaded weight |
1,941 kg (4,279 lb) |
|
Max takeoff weight |
2,095 kg (4,619 lb) |
|
Powerplant |
1× Shvetsov M-63 supercharged air-cooled radial engine,
820 kW (1,100 hp) driving a two-blade propeller |
|
Maximum speed |
525 km/h (283 kn, 326 mph) at 3,000 m (9,845 ft) |
|
Range |
700 km (378 nmi, 435 mi (with drop tanks)) |
|
Service ceiling |
9,700 m (31,825 ft) |
|
Rate of climb |
14.7 m/s (2,900 ft/min) |
|
Wing loading |
134 kg/m² (27 lb/ft²) |
|
Power/mass |
346 W/kg (0.21 hp/lb) |
|
Time to altitude |
5.8 minutes to 5,000 m (16,405 ft) |
|
Armament
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 |
|
Bombs |
200 kg
(440 lb) |
|
Built |
103 units |
|
|

Mikoyan-Gurevich MiG-3, 1941
|
Length |
8.25 m (27 ft 1 in) |
|
Wingspan |
10.20 m (33 ft 5 in) |
|
Height |
3.30 m (10 ft 9⅞ in) |
|
Wing area |
17.44 m² (188 ft²) |
|
Airfoil |
Clark YH |
|
Empty weight |
2,699 kg (5,965 lb) |
|
Loaded weight |
3,355 kg (7,415 lb) |
|
Powerplant |
1× Mikulin AM-35A liquid-cooled V-12, 993 kW (1,350 hp) |
|
Maximum speed |
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 |
|
Built |
3,172
units |
|
|

Petlyakov Pe-3, 1941
|
Crew |
2 |
|
Length |
12.66 m (41 ft 6 in) |
|
Wingspan |
17.13 m (56 ft 2 in) |
|
Wing area |
40.5 m2 (436 sq ft) |
|
Empty weight |
5,858 kg (12,915 lb) |
|
Gross weight |
8,000 kg (17,637 lb) |
|
Powerplant |
2 × Klimov M-105RA liquid-cooled V12 engines, 820 kW
(1,100 hp) each |
|
Propellers |
3-bladed |
|
Maximum speed |
530 km/h (330 mph; 290 kn) @ 5,050 meters (16,568 ft) |
|
Range |
1,500 km (932 mi; 810 nmi) |
|
Service ceiling |
9,100 m (29,856 ft) |
|
Time to altitude |
6.65 minutes to 5,000 meters (16,404 ft) |
|
Armament |
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 |
|
Bombs |
up to 700 kg (1,543 lb) |
|
Built |
360 units |
|
|

Yakovlev Yak-1, 1941
|
Length |
8.5 m (27 ft 11 in) |
|
Wingspan |
10.0 m (32 ft 10 in) |
|
Wing area |
17.2 m² (185.1 ft²) |
|
Empty weight |
2,394 kg (5,267 lb) |
|
Loaded weight |
2,883 kg (6,343 lb) |
|
Powerplant |
1× Klimov M-105PF V-12 liquid-cooled engine, 880 kW
(1,180 hp) |
|
Maximum speed |
592 km/h (368 mph) |
|
Range |
700 km (435 mi) |
|
Service ceiling |
10,050 m (32,972 ft) |
|
Rate of climb |
15.4 m/s (3,038 ft/min) |
|
Wing loading |
168 kg/m² (34 lb/ft²) |
|
Power/mass |
0.31 kW/kg (0.19 hp/lb) |
|
Armament |
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. |
|
Built |
8,700 units |
|
|

Lavochkin-Gorbunov-Gudkov
LaGG-3, 1940
|
Length |
8.81 m (28 ft 11 in) |
|
Wingspan |
9.80 m (32 ft 1.75 in) |
|
Height |
2.54 m (8 ft 4 in) |
|
Wing area |
17.4 m² (188 ft²) |
|
Empty weight |
2,205 kg (4,851 lb) |
|
Loaded weight |
2,620 kg (5,764 lb) |
|
Max takeoff weight |
3,190 kg (7,018 lb) |
|
Powerplant |
1×Klimov M-105PF liquid-cooled V-12, 924 kW (1,260 hp) |
|
Maximum speed |
575 km/h (357 mph) |
|
Range |
1000 km (621 mi) |
|
Service ceiling |
9,700 m (31,825 ft) |
|
Rate of climb |
14.9 m/s (2,926 ft/min) |
|
Wing loading |
150 kg/m² (31 lb/ft²) |
|
Power/mass |
350 W/kg (0.21 hp/lb) |
|
Armament |
1×20 mm ShVAK cannon 6× RS-82 or RS-132 rockets up a
total of 200 kg (441 lb 2× 12.7 mm (0.50 in) Berezin BS
machine guns |
|
Built |
6582 unit |
|
|

Polikarpov I-185, 1941 |
|
Length |
7.77 m (25 ft 6 in) |
|
Wingspan |
9.80 m (32 ft 2 in) |
|
Height |
2.50 m (8 ft 2 in) |
|
Wing area |
15.53 m² (167.10 ft²) |
|
Empty weight |
2,654 kg (5,840 lb) |
|
Loaded weight |
3,500 kg (7,700 lb) |
|
Powerplant |
1× Shvetsov M-71 radial engine, 1,492 kW (2,000 hp) |
|
Maximum speed |
630 km/h (391 mph) |
|
Range |
835 km (520 mi) |
|
Service ceiling |
11,000 m (36,080 ft) |
|
Rate of climb |
16.1 m/s (3,150 ft/min) |
|
Wing loading |
225 kg/m² (46 lb/ft²) |
|
Power/mass |
430 W/kg (0.26 hp/lb) |
|
Armament |
3 × 20 mm ShVAK cannons |
|
Bombs |
up to 500 kg (1,100 lb) (2 × 250 kg (551 lb) or 4 100
kg (220 lb)) or 8 RS-82 rockets |
|
|

Yakovlev Yak-3, 1943
|
Length |
8.5 m (27 ft 10 in) |
|
Wingspan |
9.2 m (30 ft 2 in) |
|
Height |
2.39 m (7 ft 11 in) |
|
Wing area |
14.85 m² (159.8 ft²) |
|
Empty weight |
2,105 kg (4,640 lb) |
|
Loaded weight |
2,692 kg (5,864 lb) |
|
Powerplant |
1× Klimov VK-105PF-2 V-12 liquid-cooled piston engine,
970 kW (1,300 hp) |
|
Maximum speed |
655 km/h (407 mph) |
|
Range |
650 km (405 miles) |
|
Service ceiling |
10,700 m (35,000 ft) |
|
Rate of climb |
18.5 m/s (3,645 ft/min) |
|
Wing loading |
181 kg/m² (36.7 lb/ft²) |
|
Power/mass |
0.36 kW/kg (0.22 hp/lb) |
|
Guns |
1 × 20 mm ShVAK cannon, 2 × 12.7 mm Berezin UBS machine
guns |
|
Built |
4,848 units |
|
|

Lavochkin La-5, 1942
|
Length |
8.67 m (28 ft 5.33 in) |
|
Wingspan |
9.80 m (32 ft 1.75 in) |
|
Height |
2.54 m (8 ft 4 in) |
|
Wing area |
17.5 m² (188 ft²) |
|
Empty weight |
2,605 kg (5,743 lb) |
|
Loaded weight |
3,265 kg (7,198 lb) |
|
Max takeoff weight |
3,402 kg (7,500 lb) |
|
Powerplant |
1× Shvetsov ASh-82FN radial engine, 1,385 kW (1,850 hp) |
|
Maximum speed |
648 km/h (403 mph) |
|
Range |
765 km (475 miles) |
|
Service ceiling |
11,000 m (36,089 ft) |
|
Rate of climb |
16.7 m/s (3,280 ft/min) |
|
Wing loading |
186 kg/m² (38 lb/ft²) |
|
Power/mass |
0.42 kW/kg (0.26 hp/lb) |
|
Armament |
2 × 20 mm ShVAK cannons,200 rpg |
|
Bombs |
up to 100 kg (220 lb) each |
|
Built |
9,920 units |
|
|

Yakovlev Yak-7, 1941
|
Length |
8.50 m (27 ft 11 in) |
|
Wingspan |
10.00 m (32 ft 10 in) |
|
Height |
2.75 m (9 ft 0 in) |
|
Wing area |
17.2 m² (185 ft²) |
|
Empty weight |
2,477 kg (5,449 lb) |
|
Loaded weight |
2,960 kg (6,512 lb) |
|
Powerplant |
1× Klimov M-105P, 783 kW (1,050 hp) |
|
Maximum speed |
560 km/h (350 mph) |
|
Range |
643 km (401 mi) |
|
Service ceiling |
9,250 m (30,340 ft) |
|
Rate of climb |
12 m/s (2,411 ft/min) |
|
Wing loading |
172.6 kg/m² (35 lb/ft²) |
|
Power/mass |
0.26 kW/kg (0.16 hp/lb) |
|
Armament |
1 × 20 mm ShVAK cannon, 2 × 7.62 mm ShKAS machine guns |
|
Built |
6,399 units |
|
|

Yakovlev Yak-9, 1942
|
|
Yak-9D |
Yak-9U |
|
Length |
28 ft (8.55 m) |
28 ft (8.55 m) |
|
Wingspan |
31 ft 11 in (9.74 m) |
31 ft 11 in (9.74 m) |
|
Height |
9 ft 10 in (3.00 m) |
9 ft 10 in (3.00 m) |
|
Wing area |
185.1 ft² (17.2 m²) |
185.1 ft² (17.2 m²) |
|
Empty weight |
5,170 lb (2,350 kg) |
5,526 lb (2,512 kg) |
|
Loaded weight |
6,858 lb (3,117 kg) |
7,049 lb (3,204 kg) |
|
Powerplant |
1× Klimov M-105 PF V-12 liquid-cooled piston engine,
1,180 hp (880 kW) |
1× Klimov VK-107A V-12 liquid-cooled piston engine,
1,500 hp (1,120 kW) |
|
Maximum speed |
367 mph at altitude (591 km/h) |
417 mph at altitude (672 km/h) |
|
Range |
845 miles (1,360 km) |
420 miles (675 km) |
|
Service ceiling |
30,000 ft (9,100 m) |
35,000 ft (10,650 m) |
|
Rate of climb |
2,690 ft/min (13.7 m/s) |
3,280 ft/min (16.7 m/s) |
|
Wing loading |
37 lb/ft² (181 kg/m²) |
38 lb/ft² (186 kg/m²) |
|
Power/mass |
0.17 hp/lb (0.28 kW/kg) |
0.21 hp/lb (0.35 kW/kg) |
|
Armament |
1 × 20 mm ShVAK cannon, 120 rounds, 1 × 12.7 mm UBS
machine gun, 200 rounds |
1 × 20 mm ShVAK cannon, 120 rounds, 2 × 12.7 mm UBS
machine guns, 170 rpg |
|
|

Lavochkin La-7 Fin, 1944
|
Length |
8.6 m (28 ft 3 in) |
|
Wingspan |
9.8 m (32 ft 2 in) |
|
Height |
2.54 m (8 ft 4 in) |
|
Wing area |
17.59 m2 (189.3 sq ft) |
|
Gross weight |
3,315 kg (7,308 lb) |
|
Powerplant |
1 × Shvetsov ASh-82FN 14-cylinder, two-row, air-cooled
radial, 1,096 kW (1,470 hp) |
|
Propellers |
3-bladed VISh-105V-4 |
|
Maximum speed |
661 km/h (411 mph; 357 kn) @ 6,000 meters (19,685 ft) |
|
Range |
665 km (413 mi; 359 nmi) (1944 model) |
|
Service ceiling |
10,450 m (34,285 ft) |
|
Time to altitude |
5.3 minutes to 5,000 meters (16,404 ft) |
|
Guns |
2 × 20 mm ShVAK cannons with 200 rounds per gun or 3 ×
20 mm Berezin B-20 cannons with 100 rpg |
|
Bombs |
200 kg (440 lb) of bombs |
|
Built |
5,753 units |
|
|

Mikoyan-Gurevich MiG-9 Fargo, 1946
|
Length |
9.83 m (32 ft 3 in) |
|
Wingspan |
10 m (32 ft 10 in) |
|
Height |
3.22 m (10 ft 7 in) |
|
Wing area |
18.20 m² (195.9 ft²) |
|
Empty weight |
3,420 kg (7,540 lb) |
|
Loaded weight |
4,965 kg (10,945 lb) |
|
Max takeoff weight |
5,500 kg (12,125 lb) |
|
Powerplant |
2× Kolesov RD-20 turbojets, 7.8 kN (1754 lbf) each |
|
Maximum speed |
Mach 0.8, 910 km/h (565 mph) at 4,500 m (14,765 ft) |
|
Range |
800 km (495 mi) |
|
Service ceiling |
13,000 m (42,650 ft) |
|
Rate of climb |
19.4 m/s (3,815 ft/min) |
|
Thrust/weight |
0.40 |
|
Armament |
1 × 37 mm NL-37 cannon, 2 × 23 mm NS-23 cannons |
|
Built |
608
units |
More → |
|

Yakovlev Yak-15, 1946
|
Length |
8.70 m (28 ft 6½ in) |
|
Wingspan |
9.20 m (30 ft 2¼ in) |
|
Height |
2.27 m (7 ft 5⅓ in) |
|
Wing area |
14.85 m² (160 ft²) |
|
Empty weight |
1,918 kg (4,228 lb) |
|
Loaded weight |
2,234 kg (5,807 lb) |
|
Powerplant |
1× Tumansky RD-10 turbojet, 8.9 kN (2,000 lbf) |
|
Maximum speed |
700 km/h (378 knots, 435 mph) at sea level, 805 km/h
(435 knots, 500 mph) at 5,000 m (16,400 ft) |
|
Range |
510 km (275 NM, 317 miles) |
|
Service ceiling |
13,350 m (43,800 ft) |
|
Wing loading |
150 kg/m² (36.3 lb/ft²) |
|
Thrust/weight |
0.34 |
|
Climb to 5,000 m (16,400 ft) |
4.8 min |
|
Armament |
2× 23 mm Nudelman-Suranov NS-23 cannon with 60 rounds
each |
|
Builtt |
208 |
More
→ |
|

Sukhoi Su-9, 1946
|
Length |
10.57 m (34 ft 8 in) |
|
Wingspan |
11.21 m (36 ft 9 in) |
|
Height |
3.72 m (12 ft 2 in) |
|
Wing area |
20.24 m² (217.87 ft²) |
|
Empty weight |
4,060 kg (8,950 lb) |
|
Loaded weight |
5,890 kg (12,990 lb) |
|
Max takeoff weight |
6,380 kg (14,070 lb) |
|
Powerplant |
2× Tumansky RD-10 turbojets, 8.8 kN (1,984 lbf) |
|
Fuel capacity |
1,750 kg (3,860 lb) |
|
Maximum speed |
885 km/h (480 kn, 550 mph) at 5,000 m (16,405 ft) |
|
Range |
1,140 km (615 nmi, 710 mi) |
|
Service ceiling |
12,800 m (41,984 ft) |
|
Rate of climb |
4.2 min to 5,000 m (16,405 ft) |
|
Wing loading |
291 kg/m² (60 lb/ft²) |
|
Thrust/weight |
0.31 |
|
Endurance |
1 hour 44 minutes |
|
Armament |
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. |
|
|

Mikoyan-Gurevich MiG-17 Fresco, 1950
|
Length |
11.36 m (37 ft 3 in) |
|
Wingspan |
9.63 m (31 ft 7 in) |
|
Height |
3.80 m (12 ft 6 in) |
|
Wing area |
22.6 m² (243.2 ft²) |
|
Empty weight |
3,930 kg (8,646 lb) |
|
Loaded weight |
5,354 kg (11,803 lb) |
|
Max takeoff weight |
6,286 kg (13,858 lb) |
|
Powerplant |
1× Klimov VK-1F afterburning turbojet, 33.1 kN with
afterburner (7,440 lbf) |
|
Maximum speed |
1,144 km/h at 3,000 m (711 mph at 10,000 ft (3,000 m)) |
|
Range |
1,080 km, 1,670 km with drop tanks (670 mi/1,035 mi) |
|
Service ceiling |
16,600 m (54,500 ft) |
|
Rate of climb |
65 m/s (12,795 ft/min) |
|
Wing loading |
237 kg/m² (48 lb/ft²) |
|
|

Yakovlev Yak-25 Flashlight-A, 1952
|
Length |
15.67 m (51 ft 5 in) |
|
Wingspan |
10.94 m (35 ft 10 in) |
|
Height |
4.4 m (14 ft 5 in) |
|
Wing area |
28.94 m² (311.51 ft²) |
|
Empty weight |
5,675 kg (12,510 lb) |
|
Loaded weight |
8,675 kg (19,125 lb) |
|
Max takeoff weight |
9,450 kg (29,760 lb) |
|
Powerplant |
2× Mikulin AM-5 (RD-5A) turbojets, 23 kN (5,000 lbf)
each |
|
Maximum speed |
1,090 km/h (680 mph) |
|
Range |
2,700 km with external tank (1,687 mi) |
|
Service ceiling |
15,200 m (50,000 ft) |
|
Rate of climb |
30 m/s (5,960 ft/min) |
|
Wing loading |
327 kg/m² (67 lb/ft²) |
|
Thrust/weight |
0.53 |
|
Guns |
2× 37 mm Nudelman NL-37 cannon (50 rounds per gun) |
|
Number built |
638 units |
|
|

Mikoyan-Gurevich MiG-19 Farmer, 1955
|
Length |
12.5 m (41 ft) |
|
Wingspan |
9.2 m (30 ft 2 in) |
|
Height |
3.9 m (12 ft 10 in) |
|
Wing area |
25.0 m² (270 ft²) |
|
Empty weight |
5,447 kg (11,983 lb) |
|
Max takeoff weight |
7,560 kg (16,632 lb) |
|
Powerplant |
2× Tumansky RD-9B afterburning turbojets, 31.9 kN
(7,178 lbf) each |
|
Fuel capacity |
1,800 kg (3,960 lb) |
|
Maximum speed |
1,455 km/h (909 mph) |
|
Range |
685 km (1,375 mi) |
|
Service ceiling |
17,500 m (57,400 ft) |
|
Rate of climb |
180 m/s (35,425 ft/min) |
|
Wing loading |
302.4 kg/m² (61.6 lb/ft²) |
|
Thrust/weight |
0.86 |
|
Guns |
3x 30 mm NR-30 cannons (75 rounds per gun for wing
guns, 55 rounds for the fuselage gun) |
|
Hardpoints |
4 underwing pylons and provisions to carry
combinations of |
|
Rockets |
unguided rockets |
|
Missiles |
4 Vympel K-13 AAMs |
|
Bombs |
Up to 250 kg (550 lb) of bombs |
|
|

Yakovlev Yak-25 Flashlight-C, 1958
|
Length |
18.55 m (60 ft 10 in) |
|
Wingspan |
11.82 m (38 ft 9 in) |
|
Wing area |
28.94m² (311.5ft²) |
|
Empty weight |
6893 kg (15,165 lb) |
|
Loaded weight |
10,700 kg (23,540 lb) |
|
Max takeoff weight |
13,600 kg (30,000 lb) |
|
Powerplant |
2×Tumansky RD-9F , 37.2 kN (8,360 lbf) each |
|
Maximum speed |
1,285 km/h (803 mph) |
|
Range |
2,380 km (1,488 miles) |
|
Service ceiling |
16,550 m (54,284 ft) |
|
Rate of climb |
m/s (ft/min) |
|
Wing loading |
kg/m² (lb/ft²) |
|
Armament |
1x 23 mm Nudelman-Rikhter NR-23 cannon |
|
Number built |
166 |
|
|

Sukhoi Su-9 Fishpot, 1958
|
Length |
18.055 m (59 ft 2⅞ in) |
|
Wingspan |
8.536 m (28 ft) |
|
Height |
4.82 m (15 ft 9¾ in) |
|
Wing area |
34 m² (365.5 ft²) |
|
Empty weight |
7,675 kg (16,920 lb) |
|
Loaded weight |
11,412kg (25,225 lb) |
|
Max takeoff weight |
12,512kg (37,583 lb) |
|
Powerplant |
1× Lyulka AL-7F1-100U turbojet |
|
Dry thrust |
66.7 kN (14,990 lbst) |
|
Thrust with afterburner |
94.2 kN (21,160 lbst) |
|
Maximum speed |
Mach 2.0, 2,230 km/h (1,385 mph) @ 12,000m(39,370ft)
for one minute |
|
Range |
1,350km (838 miles) |
|
Service ceiling |
20,000 m (65,620 ft) |
|
Rate of climb |
136.7 m/s (27,000 ft/min) |
|
Wing loading |
383 kg/m² (74 lb/ft²) |
|
Missiles |
4 × K-5MS (AA-1 'Alkali') air-to-air missiles |
|
|

Tupolev Tu-28/Tu-128 Fiddler, 1959
|
Crew |
Two, pilot and radar operator |
|
Length |
27.2 m (89 ft) |
|
Wingspan |
18.1 m (59 ft) |
|
Height |
7.0 m (23 ft) |
|
Wing area |
80 m² (861 ft²) |
|
Empty weight |
24,500 kg (54,013 lb) |
|
Loaded weight |
40,000 kg (88,185 lb) |
|
Powerplant |
2× Lyulka AL-7F-2 turbojet, 107.9 kN (24,300 lbf) each |
|
Maximum speed |
Mach 1.65 at high altitude (1,740
km/h, 1,089 mph) |
|
Range |
3,200 km (2,000 mi) |
|
Service ceiling |
18,000 m (59,055 ft) |
|
Rate of climb |
125 m/s (24,600 ft/min) |
|
Wing loading |
500 kg/m² (102 lb/ft²) |
|
Thrust/weight |
0.55 |
|
Missiles |
4 × Bisnovat R-4 air-to-air missiles
(usually 2 × radar-guided R-4R and 2 × infrared-homing
R-4T) |
|
|

Mikoyan-Gurevich MiG-21 Fishbed, 1959
|
Length |
15.76 (with
pitot tube) m (51 ft 8.47 in) |
|
Wingspan |
7.154 m (23 ft
5.66 in) |
|
Height |
4.1 m (13 ft
5.41 in) |
|
Wing area |
23.0 m² (247.3
ft²) |
|
Empty weight |
4,871 kg
(10,738 lb) |
|
Gross weight |
7,100 kg
(15,650 lb) |
|
Powerplant |
1 × Tumanskiy
R11F-300, 37.27 kN (8,380 lbf) thrust dry, 56.27 kN
(12,650 lbf) with afterburner each |
|
Maximum speed |
2,125 km/h
(1,385 mph, Mach 2.05) |
|
Range |
1,580 km (981
miles) |
|
Service ceiling |
19,000 m
(62,335 ft) |
|
Guns |
1x internal 30
mm NR-30 cannon |
|
Missiles |
2x K-13 or
K-13A (R-3S) AAM or |
|
Bombs |
2x 500 kg
(1,102 lbs) of bombs |
|
|
.jpg)
Yakovlev Yak-28 Firebar, 1958
|
Length |
21.6 m (75 ft 0
in) |
|
Wingspan |
12.50 m (41 ft
0 in) |
|
Height |
3.95 m (12 ft
11 in) |
|
Wing area |
37.6 m² (405
ft²) |
|
Empty weight |
9,970 kg
(21,980 lb) |
|
Loaded weight |
15,000 kg
(33,069 lb) |
|
Max takeoff
weight |
20,000 kg
(44,092 lb) |
|
Powerplant |
2× Tumansky
R-11 afterburning turbojets, 46 kN dry, 62 kN with
afterburning (10,140 lbf dry, 13,670 lbf with
afterburning) each |
|
Maximum speed |
1840 km/h (1142
mph) |
|
Range |
2,500 km (1,550
mi) |
|
Service ceiling |
16,750 m
(54,954 ft) |
|
Wing loading |
531 kg/m²
(108.6 lb/ft²) |
|
Armament |
2 × R-98M (AA-3
'Anab') air-to-air missiles, usually one R-98TM infrared
and one R-98RM semi-active radar homing? 2 × K-13A (AA-2
'Atoll') short-range missiles (occasionally fitted) |
|
|

Sukhoi Su-15 Flagon, 1967
|
Length |
19.56 m (64 ft
2 in) |
|
Wingspan |
9.34 m (30 ft 7
in) |
|
Height |
4.84 m (15 ft
10 in) |
|
Wing area |
36.6 m² (394
ft²) |
|
Empty weight |
10,874 kg
(23,973 lb) |
|
Loaded weight |
17,194 kg
(37,920 lb) |
|
Powerplant |
2× Tumansky
R-13F2-300 turbojets |
|
Dry thrust |
40.21 kN (9,040
lbf) each |
|
Thrust with
afterburner |
70.0 kN (15,730
lbf) each |
|
Maximum speed |
Mach 2.1, 2,230
km/h (1,386 mph) armed (2 AA-3 no ext tanks) at high
altitude |
|
Combat |
1,380 km (897
mi) |
|
Ferry |
1,700 km (1,106
mi) |
|
Service ceiling |
18,100 m
(59,383 ft) |
|
Rate of climb |
228 m/s (45,000
ft/min) |
|
Wing loading |
102.4 lb/ft²
(555 kg/m²) |
|
Armament |
2 × R-98M/AA-3
Anab (outer wing pylons), 2 × or 4 × R-60/AA-8 Aphid
(inner pylons),Option of 2 × UPK-23-250 23 mm gun pods
on fuselage pylons |
|
|

Mikoyan-Gurevich MiG-23 Flogger, 1967
|
Length |
16.70 m (56 ft
9.5) |
|
Wingspan |
Spread, 13.97 m
(45 ft 10 in) |
|
Height |
4.82 m (15 ft
9.75 in) |
|
Wing area |
37.35 m²
spread, 34.16 m² swept (402.05 ft² / 367.71 ft²) |
|
Empty weight |
9,595 kg
(21,153 lb) |
|
Loaded weight |
15,700 kg
(34,612 lb) |
|
Max takeoff
weight |
18,030 kg
(39,749 lb) |
|
Powerplant |
1× Khatchaturov
R-35-300 afterburning turbojet, 83.6 kN dry, 127 kN
afterburning (18,850 lbf / 28,700 lbf) |
|
Maximum speed |
Mach 2.32,
2,445 km/h at altitude; Mach 1.14, 1,350 km/h at sea
level (1,553 mph / 840 mph) |
|
Range |
1,150 km with
six AAMs combat, 2,820 km ferry (570 mi / 1,750 mi) |
|
Service ceiling |
18,500 m
(60,695 ft) |
|
Rate of climb |
240 m/s (47,245
ft/min) |
|
Wing loading |
420 kg/m² (78.6
lb/ft²) |
|
Thrust/weight |
0.88 |
|
Armament |
1x
Gryazev-Shipunov GSh-23L 23 mm cannon with 200 rounds.
Two fuselage, two wing glove, and two wing pylons for up
to 3,000 kg (6,610 lb) of stores |
|
|

Mikoyan-Gurevich MiG-25 Foxbat, 1964
|
Length |
19.75 m (64 ft
10 in) |
|
Wingspan |
14.01 m (45 ft
11.5 in) |
|
Height |
6.10 m (20 ft
0.25 in) |
|
Wing area |
61.40 m²
(660.93 ft²) |
|
Empty weight |
20,000 kg
(44,080 lb) |
|
Loaded weight |
36,720 kg
(80,952 lb) |
|
Powerplant |
2× Tumansky
R-15B-300 afterburning turbojets |
|
Dry thrust |
73.5 kN (16,524
lbf) each |
|
Thrust with
afterburner |
100.1 kN
(22,494 lbf) each |
|
Maximum speed |
|
High altitude |
Mach 3.2
(3,500 km/h, 2,170 mph); Mach 2.83 (3,200 km/h, 1,920
mph) continuous engine limit |
|
Low altitude |
1,200 km/h (650
knots, 740 mph) |
|
Range |
1,730 km (935
nmi, 1,075 mi) with internal fuel |
|
Ferry range |
2,575 km (1,390
nmi) |
|
Service ceiling |
20,700 m (with
four missiles) (67,915 ft; over 80,000 ft (24.4 km) for
RB models) |
|
Rate of climb |
208 m/s (40,950
ft (12,480 m) / min) |
|
Wing loading |
598 kg/m²
(122.5 lb/ft²) |
|
Thrust/weight |
0.41 |
|
Time to altitude |
8.9 min to
20,000 m (65,615 ft) |
|
Armament |
2x radar-guided
R-40R (AA-6 "Acrid") air-to-air missiles, and 2x
infrared-guided R-40T missiles |
|
|
Yakovlev Yak-38 VTOL fighter
Forger, 1971
|
Length |
16.37 m (50 ft
1 in) |
|
Wingspan |
7.32 m (24 ft 0
in) |
|
Height |
4.25 m (14 ft 5
in) |
|
Wing area |
18.5 m² (199
ft²) |
|
Empty weight |
7,385 kg
(16,281 lb) |
|
Loaded weight |
kg (lb) |
|
Max takeoff
weight |
11,300 kg
(28,700 lb) |
|
Powerplant |
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. |
|
|

Mikoyan-Gurevich MiG-29 Fulcrum, 1977
|
Length |
17.37 m (57 ft) |
|
Wingspan |
11.4 m (37 ft 3
in) |
|
Height |
4.73 m (15 ft 6
in) |
|
Wing area |
38 m² (409 ft²) |
|
Empty weight |
11,000 kg
(24,250 lb) |
|
Loaded weight |
16,800 kg
(37,000 lb) |
|
Max takeoff
weight |
21,000 kg
(46,300 lb) |
|
Powerplant |
2× Klimov RD-33
afterburning turbofans, 8,300 kgf (81.4 kN, 18,300 lbf)
each |
|
Maximum speed |
Mach 2.25
(2,400 km/h, 1,490 mph) At low altitude Mach 1.25 (1,500
km/h, 930 mph) |
|
Range |
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. |
|
|

Sukhoi Su-30 Flanker-С, 1989
|
Crew |
2 |
|
Length |
21.935 m (72.97 ft) |
|
Wingspan |
14.7 m (48.2 ft) |
|
Height |
6.36 m (20.85 ft) |
|
Wing area |
62.0 m² (667 ft²) |
|
Empty weight |
17,700 kg (39,021 lb) |
|
Loaded weight |
24,900 kg (54,900 lb) |
|
Max takeoff weight |
34,500 kg (76,060 lb) |
|
Powerplant |
2× AL-31FL
low-bypass turbofans |
|
Dry thrust |
7,600 kgf (74.5 kN, 16,750 lbf)
each |
|
Thrust with afterburner |
12,500 kgf (122.58 kN, 27,560 lbf)
each |
|
Maximum speed |
Mach 2.0 (2,120 km/h, 1,320 mph) |
|
Range |
3,000 km (1,620 nmi) at altitude |
|
Service ceiling |
17,300 m (56,800 ft) |
|
Rate of climb |
230 m/s (45,275 ft/min) |
|
Wing loading |
401 kg/m² (82.3 lb/ft²) |
|
Thrust/weight |
1.0 |
|
Guns |
1 × GSh-30-1
gun (30 mm caliber, 150 rounds) |
|
AAMs |
6 × R-27ER1 (AA-10C), 2 × R-27ET1
(AA-10D), 6 × R-73E (AA-11), 6 × R-77 RVV-AE(AA-12) |
|
ASMs |
6 ×
Kh-31P/Kh-31A anti-radar missiles, 6 × Kh-29T/L laser
guided missiles, 2 × Kh-59ME |
|
Aerial bombs |
6 × KAB 500KR,
3 × KAB-1500KR, 8 × FAB-500T, 28 × OFAB-250-270 |
|
|

Sukhoi Su-33 Flanker-F, 1985
|
Length |
21.94 m (72 ft) |
|
Wingspan |
14.70 m (48.25
ft) |
|
Height |
5.93 m (19.5
ft) |
|
Wing area |
62.0 m² (667
ft²) |
|
Empty weight |
18,400 kg
(40,600 lb) |
|
Loaded weight |
29,940 kg
(66,010 lb) |
|
Max takeoff
weight |
33,000 kg
(72,750 lb) |
|
Powerplant |
2× AL-31F
afterburning turbofans |
|
Dry thrust |
7,600 kgf (74.5
kN, 16,750 lbf) each |
|
Thrust with
afterburner |
12,500 kgf
(122.6 kN, 27,560 lbf) each |
|
Wingspan, wings
folded |
7.40 m (24.25
ft) |
|
Maximum speed |
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 |
|
Cruise speed |
1,850 - 2,100 km/h (1,150 - 1,300 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/ft ²) |
|
Thrust/weight |
1.19 |
|
Maximum g-load |
10-11 g |
|
Guns |
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 |
|
|
| |