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A-144  1
2
3
| Functin: | Flying test-bed |
| Crew: | 1 |
| Year: | 1968 |
| Powerplant: | One R-13F-300 afterburning turbojet |
| Wing span: | 26 ft. 7 in. (27 ft. 7 in.) | 8,15 m. (11,5) m. |
| Lenght: | 40 ft. 3 in. | 12.29 m. |
| Height: | 15 ft. 4 in. | 4.71 m. |
| Weight |
| Max. take off: | 19,800 lb. | 9,000 kg. |
| Ceiling: | 65,600 ft. | 20,000 m. |
| Speed: | 1,304 mph. | 2,100 km/h. |
I-1
| Function | Front-line fighter |
| Crew: | 1 |
| Year: | 1956 |
| Powerplant | One Klimov VK-3 afterburning turbojet |
| Thrust: | 18,480 lb. | 8,400 kg. |
| Wing span: | 29 ft. 5 in. | 9.00 m. |
| Lenght: | 41 ft. 7 in. | 12.70 m. |
| Weight |
| Empty: | 11,189 lb. | 5,086 kg. |
| Ceiling: | 55,760 ft. | 17,000 m. |
| Speed: | 1,217 mph. | 1,960 km/h |
I-3U
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1956 |
| Powerplant | One Klimov VK-3 afterburning turbojet |
| Thrust: | 18,480 lb. | 8,400 kg. |
| Ceiling: | 59,040 ft. | 18,000 m. |
| Speed: | 1,217 mph. | 1,960 km/h |
| Range: | 1,118 miles | 1,800 km. |
I-7U
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1957 |
| Powerplant: | One Lyulka AL-7F afterburning turbojet |
| Wing span: | 32 ft. 7 in. | 9.98 m. |
| Lenght: | 55 ft. 5 in. | 16.92 m. |
| Weight |
| Empty: | 17,494 lb. | 7,952 kg. |
| Max. take off | 25,388 lb. | 11,540 kg. |
| Speed: | 1,031 mph. | 1,660 km/h. |
| Range: | 935 miles | 1,505 km. |
I-75
1
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1958 |
| Powerplant: | One Lyulka AL-7F-1 afterburning turbojet |
| Thrust: | 20,273 lb. | 9,215 kg. |
| Wing span: | 32 ft. 7 in. | 9.98 m. |
| Lenght: | 59 ft. 9 in. | 18.27 m. |
| Weight |
| Empty: | 18,203 lb. | 8,274 kg. |
| Speed: | Mach 2.5 |
I-210
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1941 |
| Powerplant: | One 1,700 hp. Shvetsov M-82A 12-cylinder liquid-cooled engine |
| Wing span: | 33 ft. 5 in. | 10.20 m. |
| Lenght: | 26 ft. 5 in. | 8.08 m. |
| Weight |
| Empty: | 5,984 lb. | 2,720 kg. |
| Speed: | 351 mph. | 565 km/h |
| Range: | 665 miles | 1,070 km. |
I-211
1
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1942 |
| Powerplant: | One 1,850 hp. Shvetsov M-82FN 12-cylinder liquid-cooled engine |
| Wing span: | 33 ft. 5 in. | 10.20 m. |
| Lenght: | 26 ft. 1 in. | 7.95 m. |
| Height: | 11 ft. 9 in. | 3.63 m. |
| Weight |
| Empty: | 5,562 lb. | 2,528 kg. |
| Max. take off: | 6,820 lb. | 3,100 kg. |
| Ceiling: | 37,064 ft. | 11,300 m. |
| Speed: | 416 mph. | 670 km/h |
| Range: | 708 miles | 1,140 km. |
I-225 (A)
1
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1944 |
| Powerplant: | One 2,200 hp. Mikulin AM-42FB 12-cylinder liquid-cooled engine |
| Wing span: | 36 ft. 1 in. | 11.00 m. |
| Lenght: | 31 ft. 5 in. | 9.60 m. |
| Height: | 12 ft. 1 in. | 3.70 m. |
| Weight |
| Empty: | 6,622 lb. | 3,010 kg. |
| Speed: | 451 mph. | 726 km/h |
I-230
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1942 |
| Powerplant: | One 1,350 hp. Mikulin AM-35A 12-cylinder liquid-cooled engine |
| Wing span: | 33 ft. 5 in. | 10.20 m. |
| Lenght: | 28 ft. 3 in. | 8.62 m. |
| Weight |
| Empty: | 5,746 lb. | 2,612 kg. |
| Max. take off: | 7,227 lb. | 3,285 kg. |
| Speed: | 410 mph. | 660 km/h. |
| Range: | 839 miles | 1,350 km. |
I-231
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1943 |
| Powerplant: | One 1,700 hp. Mikulin AM-39 12-cylinder liquid-cooled engine |
| Wing span: | 33 ft. 5 in. | 10.20 m. |
| Lenght: | 28 ft. 3 in. | 8.62 m. |
| Weight |
| Empty: | 5,683 lb. | 2,583 kg. |
| Max. take off: | 7,231 lb. | 3,287 kg. |
| Speed: | 439 mph. | 707 km/h. |
| Range: | 839 miles | 1,350 km. |
I-270 (ZH)
1
2
3
| Function: | Target-defence fighter |
| Crew: | 1 |
| Year: | 1947 |
| Powerplant: | One RD-2M-3V rocked engine |
| Thrust: | 3,190 lb. | 1,450 kg. |
| Wing span: | 25 ft. 4 in. | 7.75 m. |
| Lenght: | 29 ft. 2 in. | 8.91 m. |
| Height: | 10 ft. 1 in. | 3.08 m. |
| Weight |
| Empty: | 3,401 lb. | 1,546 kg. |
| Max. take off: | 9,064 lb. | 4,120 kg. |
| Ceiling: | 59,040 ft. | 18.000 m. |
| Speed: | 621 mph. | 1,000 km/h. |
| Range: | Nine minutes and three seconds power |
I-320 (R)
1
2
| Function: | All-wheater fighter |
| Crew: | 1 |
| Year: | 1950 |
| Powerplant: | Two Klimov RD-45F |
| Thrust: | 4,994 lb. | 2,270 kg. each |
| Wing span: | 46 ft. 6 in. | 14.20 m. |
| Lenght: | 51 ft. 7 in. | 15.77 m. |
| Weight |
| Max. take off: | 26,609 lb. | 12,095 kg. |
| Ceiling: | 49,528 ft. | 15,100 m. |
| Speed: | 677 mph. | 1,090 km/h. |
| Range: | 749 miles | 1,205 km. |
I-350
1
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1953 |
| Powerplant: | One Lyulka TR-3 afterburning turbojet |
| Thrust: | 10,120 lb. | 4,600 kg. |
| Wing span: | 31 ft. 9 in. | 9,73 m. |
| Lenght: | 54 ft. 6 in. | 16.65 m. |
| Weight |
| Empty: | 13,475 lb. | 6,125 kg. |
| Max. take off: | 19,162 lb. | 8,710 kg. |
| Speed: | 770 mph. | 1,240 km/h. |
| Range: | 696 miles | 1,120 km. |
I-360
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1952 |
| Powerplant: | Two Mikulin AM-5F afterburning turbojet |
| Thrust: | 5,940 lb. | 2,700 kg. each |
| Wing span: | 29 ft. 7 in. | 9.04 m. |
| Lenght: | 45 ft. 6 in. | 13.90 m. |
| Height: | 12 ft. | 3.95 m. |
MiG-2000
1
2
| Function: | Single-stage space vehicle |
| Year: | 1993 |
| Powerplant: | Ramjet + liquid-propellant |
| Core diameter: | 63 ft. 6 in. | 19.7 m. |
| Lenght: | 177 ft. 4 in. | 54.1 m. |
| Weight |
| Max. take off: | 660,000 lb. | 300,000 kg. |
| Payload: | 19,800 lb. | 9,000 kg. |
| Orbit: | 124 miles | 200 km. |
| Ceiling: | 65,600 ft. | 20,000 m. |
Max. speed at
athmosphere: | Mach 5 |
| Re-entry cross-range: | 1,863 miles | 3,000 km. |
SM-12PM
1
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1957 |
| Powerplant: | Two Sorokin R3-26 afterburning turbojets |
| Thrust: | 7,920 lb. | 3,600 kg. each |
| Ceiling: | 57,072 ft. | 17,400 m. |
| Speed: | 1,068 mph. | 1,720 km/h |
| Range: | 1,056 miles | 1,700 km. |
SN
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1953 |
| Powerplant: | One VK-1A afterburning turbojet |
| Thrust: | 6,380 lb. | 2,900 kg. |
| Wing span: | 31 ft. 6 in. | 9.63 m. |
| Lenght: | 40 ft. 4 in. | 12.33 m. |
| Height: | 12 ft. 5 in. | 3.80 m. |
| Weight |
| Empty: | 9,134 lb. | 4,152 kg. |
| Max. take off: | 12,364 lb. | 5,620 kg. |
| Ceiling: | 47,560 ft. | 14,500 m. |
| Speed: | 657 mph. | 1,058 km/h. |
Type 301
1
| Function: | Reconnaissance and bomber |
| Year: | early 1990s (?) |
| Powerplant: | Ramjet + turbojet |
| Weight |
| Max. take off: | 176,000 lb. | 80,000 kg. |
| Ceiling: | 82,000 - 88,560 ft. | 25,000 - 27,000 m. |
| Speed: | 2,640 mph. | 4,250 km/h. |
Type 7.01
1
2
| Function: | Supersonic interceptor |
| Crew: | 2 |
| Powerplant: | Two turbofan |
| Wing span: | 62 ft. 3 in. | 19 m. |
| Lenght: | 98 ft. 4 in. | 30 m. |
| Weight |
| Max. take off: | 143,000 lb. | 65,000 kg. |
| Speed: | 1,429 - 1,553 mph. | 2,300 - 2,500 km/h. |
| Range: | 4,348 miles | 7,000 km. |
Ye-2
1
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1955 |
| Powerplant: | One AM-9B afterburning turbojet |
| Thrust: | 7,150 lb. | 3,250 kg. |
| Wing span: | 26 ft. 6 in. | 8.11 m. |
| Lenght: | 43 ft. 4 in. | 13.23 m. |
| Weight |
| Empty: | 9,548 lb. | 4,340 kg. |
| Max. take off: | 13,750 lb. | 6,250 kg. |
| Ceiling: | 59,040 ft. | 18,000 m. |
| Speed: | 1,180 mph. | 1,900 km/h. |
| Range: | 1,242 miles | 2,000 km. |
Ye-8
1
2
3
4
5
6
7
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1962 |
| Powerplant: | One Metskhvarisvili R-21 afterburning turbojet |
| Thrust: | 15,900 lb. | 7,227 kg. |
| Wing span: | 23 ft. 5 in. | 7.15 m. |
| Lenght: | 48 ft. 9 in. | 14.90 m. |
| Weight |
| Max. take off: | 18,040 lb. | 8,200 kg. |
| Ceiling: | 65,600 ft. | 20,000 m. |
| Speed: | 1,385 miles | 2,230 km. |
Ye-23DPD
1
2
3
4
5
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1966 |
| Powerplant: | One Lyulka AL-7F afterburning turbojet |
| Thrust: | 22,000 lb. | 10,000 kg. |
Ye-50/1
1
2
3
4
5
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1956 |
| Powerplant: | One Tumansky AM-9Ye turboyet and one Dushkin S-155 rocked engine |
| Thrust: | 8,360 lb. / 2,860 lb. | 3,800 kg. / 1,300 kg. |
| Wing span: | 26 ft. 6 in. | 8.11 m. |
| Lenght: | 44 ft. 7 in. | 13.62 m. |
| Ceiling: | 75,440 ft. | 23,000 m. |
| Speed: | 1,528 mph. | 2,460 km/h. |
| Range: | 280 miles | 450 km. |
Ye-150
1
2
3
| Function: | All-weather interceptor-fighter |
| Crew: | 1 |
| Year: | 1958 |
| Powerplant: | One R-15-300, or R-15M-300 afterburning turbojet |
| Wing span: | 27 ft. 8 in. | 8.49 m. |
| Lenght: | 59 ft. 5 in. | 18.14 m. |
| Weight |
| Empty: | 18,207 lb. | 8,276 kg. |
| Max. take off: | 27,357 lb. | 12,435 kg. |
| Ceiling: | 76,260 ft. | 23,250 m. |
| Speed: | 1,795 mph. | 2,890 km/h. |
| Range: | 932 miles | 1,500 km. |
Ye-152A
1
2
3
4
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1959 |
| Powerplant: | Two Tumansky R-11F-300 afterburning turbojets |
| Thrust: | 12,628 lb. | 5,740 kg. each |
| Wing span: | 27 ft. 8 in. | 8.49 m. |
| Lenght: | 62 ft. 3 in. | 19.00 m. |
| Weight |
| Max. take off: | 30,712 lb. | 13,960 kg. |
| Ceiling: | 64,944 ft. | 19,800 m. |
| Speed: | 1,553 mph. | 2,500 km/h. |
| Range: | 1,429 miles | 2,300 km. |
Ye-152/2
| Function: | Front-line fighter |
| Crew: | 1 |
| Year: | 1961 |
| Powerplant: | One Tumansky R-15-300 afterburning turbojets |
| Thrust: | 22,462 lb. | 10,210 kg. |
| Wing span: | 28 ft. 8 in. | 8.79 m. |
| Lenght: | 64 ft. 5 in. | 19.66 m. |
| Weight |
| Empty: | 23,980 lb. | 10,900 kg. |
| Max. take off: | 31,570 lb. | 14,350 kg. |
| Ceiling: | 74,358 ft. | 22,670 m. |
| Speed: | 1,559 mph. | 2,510 km/h. |
| Range: | 913 miles | 1,470 km. |
K-9 (AA-"Awl") AAMs.
1
2
| Year: | 1961 |
| Engine: | PRD-56 |
| Tracking system: | Semiactive Radarhoming |
| Lenght: | 14 ft. 1 in. | 4.30 m. |
| Weight: | 539 lb. | 245 kg. |
| Werhead weight: | 59 lb. | 27 kg. |
| Speed: | 3,106 mph. | 5,000 km/h. |
| Launch range: | 6 miles | 9 km. |
Kh-20 (AS-3 "Kangaroo") ASMs.
1
2
| Year: | 1958 |
| Engine: | AL-7FK turbojet |
| Tracking system: | Autopilot with command guidance |
| Wing span: | 30 ft - 30 ft. 8 in. | 9.15 - 9.40 m. |
| Lenght: | 49 ft. | 14.95 m. |
| Launching weight: | 25,520 - 25,960 lb. | 11600 - 11800 kg. |
| Warhead: | 800 kT. nuclear warhead |
Kh-20M (AS-3 "Kangaroo") ASMs.
| Year: | 1959 |
| Engine: | AL-7FK turbojet |
| Tracking system: | Autopilot with command guidance |
| Wing span: | 29 ft. 7 in. | 9.04 m. |
| Lenght: | 49 ft. 1 in. | 14.96 m. |
| Launching Weight: | 24,200 lb. | 11,000 kg. |
| Warhead: | nuclear (up to 3 Mt.) or conventional warhead |
| Ceiling: | 56,600 ft. | 20,000 m. |
| Speed: | 1,149 mph. | 1,850 km/h. |
Kh-22 (AS-4 "Kitchen") ASMs.
1
2
3
4
| Year: | 1962 |
| Engine: | R-201-300 liquid-propellant |
| Tracking system: | Active radar or passive infra-red homing |
| Wing span: | 9 ft. 8 in. | 3 m. |
| Lenght: | 37 ft. 1 in. | 11.3 m. |
| Launching Weight: | 12,980 lb. | 5,900 kg. |
| Warhead weight: | 1000 kg. (2,200 lb.) conventional weahead or, 350 kT. nuclear warhead |
| Ceiling: | 78,720 ft. | 24,000 m. |
| Speed: | 1,677 - 1,863 mph. | 2,700 - 3,000 km/h. |
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