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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Бронирование фотостудий


CONTENTS:

 

MOSCOW: 

everything about

the Russian capital

 

 

More→

 

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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

 

Золотые 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?

 

 

Зарплаты, в Российской империи, СССР и Российской  Федерации с 1853 по 2010 годы

Курс рубля к доллару и доллара к рублю с 1792 по 2010

 

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

 

about Russian fighters

 

 

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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

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

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

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)

yak25-c2.jpg (600×163)

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

mig19-c1.jpg (600×162)

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

su9-c1.jpg (600×161)

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

tu128-10.jpg (600×152)

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

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.

su30-c1.jpg (600×158)

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