air-launched anti-tank guided missiles (typically launched from helicopters)
air-launched cruise missiles
air-launched anti-ship missiles
air-launched cruise missiles
air-launched anti-ship missiles
Name
|
Year
|
Weight
|
Warhead
|
Range
|
Speed
|
Propulsion
|
launched by
|
2013[3]
|
?
|
?
|
?
|
?
|
liquid fuel
|
Surface
| |
1943
|
1362 kg
|
320 kg
|
5 km
|
1235 km/h
|
none
|
Air
| |
1943
|
1045 kg
|
295 kg
|
5.0 km
|
828 km/h
|
Liquid-propellant, then gliding
|
Air
| |
1960
|
76 kg
|
28 kg
|
7 km
|
370 km/h
|
solid-fueled
|
Air, surface
| |
1985
|
582 kg
|
450 kg
|
25 km
|
1,100 km/h
|
solid-fueled
|
Air
| |
1983
|
145 kg
|
28 kg
|
25 km
|
950 km/h
|
solid fuel
|
Air
| |
1972
|
300 kg
|
140 kg
|
30 km
|
1,150 km/h
|
Solid propellant
|
Air,
| |
1955
|
600 kg
|
300 kg
|
32 km
|
subsonic
|
solid propellant
|
Air
| |
1991
|
630 kg
|
220 kg
|
35 km
|
1101 km/h
|
rocket
|
Air
| |
1943
|
2140 kg
|
1200 kg
|
36 km
|
630 km/h
|
Solid-propellant
|
Air
| |
1942
|
1000 kg
|
727 kg
|
37 km
|
260–390 km/h
|
None
|
Air
| |
1978
|
537.5 kg
|
150 kg
|
40 km
|
?
|
solid-fuel rocket
|
Air, surface
| |
KSShch (SS-N-1 SCRUBBER)
|
1958
|
2300 kg
|
nuclear
|
40 km
|
1150 km/h)
|
liquid-fuel rocket
|
Surface
|
1982
|
600 kg
|
150 kg
|
50 km
|
?
|
turbojet
|
Air
| |
1972
|
385 kg
|
130 kg
|
55+ km
|
1468 km/h
|
Solid propellant
|
Air, surface, sub
| |
1962
|
522 kg
|
150 kg
|
60 km
|
840 km/h
|
solid-fuel rocket
|
Air, surface
| |
1984
|
550 kg
|
150 kg
|
60 km
|
1070 km/h
|
solid propellant
|
Air
| |
P-70 Ametist(SS-N-7 STARBRIGHT)
|
1968
|
3500 kg
|
500 kg
|
65 km
|
1050 km/h
|
solid rocket
|
sub
|
1966
|
?
|
?
|
70 km
|
subsonic
|
turbojet
|
surface
| |
P-15 Termit(SS-N-2 STYX)
|
1958
|
3100 kg
|
454 kg
|
80 km
|
1100 km/h
|
Liquid fuel rocket
|
Surface
|
1985
|
580 kg
|
230 kg
|
110+ km
|
1000 km/h
|
Turbojet
|
Air
| |
P-120 Malakhit(SS-N-9 SIREN)
|
1972
|
2953 kg
|
500 kg
|
110 km
|
1101
|
Turbojet, solid fuel
|
Surface
|
Moskit (SS-N-22 SUNBURN)
|
1970
|
4500 kg
|
320 kg
|
120 km
|
3600 km/h
|
ramjet
|
Surface, Air
|
Kh-35 (AS-20 KAYAK)
|
1983
|
520 kg
|
145 kg
|
130 km
|
970 km/h
|
turbofan
|
Surface, Air
|
1991
|
510 kg
|
260 kg
|
150 km
|
?
|
turbojet
|
Air
| |
?
|
900 kg
|
?
|
150 km
|
?
|
ramjet
|
Air
| |
Hae Sung-I(SSM-700K)
|
2005
|
718 kg
|
300 kg
|
150 km
|
1013 km/h
|
Turbojet
|
Ship, Surface
|
1993
|
530 kg
|
?
|
170 km
|
?
|
turbojet
|
Air
| |
1979
|
670 kg
|
165 kg
|
180 km
|
1134 km/h
|
solid propellant
|
Air, surface, sub
| |
1977
|
770 kg
|
210 kg
|
180+ km
|
1116 km/h
|
Turbojet
|
Surface,Air(Perú)
| |
2009
|
410 kg
|
125 kg
|
185 km
|
high subsonic
|
turbojet and solid fuel booster
|
Air, surface
| |
2006
|
600 kg
|
230 kg
|
185+ km
|
1153 km/h
|
Turbojet
|
Air
| |
1985
|
800 kg
|
200 kg
|
200 km
|
1101 km/h
|
turbojet
|
Air, surface
| |
1943
|
730 kg
|
435 kg
|
210 km
|
450 km/h (280 mph)
|
none
|
Air
| |
1977
|
691 kg
|
221 kg
|
280 km
|
864 km/h
|
turbojet engine
|
Air, surface, sub
| |
2006
|
2500 kg (air), 3000 kg (ground)
|
300 kg
|
290 km
|
3675 km/h
|
ramjet
|
Ship,Surface, Air,Sub
| |
P-800 Oniks(SS-N-26)
|
1983
|
3000 kg
|
250 kg
|
300 km
|
3600 km/h
|
ramjet
|
Surface, Air
|
3M-54 Klub(SS-N-27 SIZZLER)
|
1993
|
1300–2300 kg
|
400 kg
|
300 km
|
735–3675 km/h
|
Turbojet
|
Surface, Sub
|
Kh-15 (AS-16 Kickback)
|
1988
|
1200 kg
|
150 kg conventional/nuclear
|
300 km
|
6200 km/h
|
solid-fuel rocket
|
Air
|
Kh-22 (AS-4 Kitchen)
|
1962
|
5820 kg
|
1000 kg conventional/nuclear
|
400 km
|
4000 km/h
|
liquid-fuel rocket
|
Air
|
1983
|
1200 kg
|
450 kg
|
450 km
|
880 km/h
|
turbofan
|
Air, surface, sub
| |
P-500 Bazalt(SS-N-12 SANDBOX)
|
1975
|
4500 kg
|
1000 kg
|
550 km
|
3060 km/h
|
liquid fuel rocket
|
surface/submerged
|
P-5 Pyatyorka(SS-N-3 SHADDOCK)
|
1959
|
5000 kg
|
1000 kg
|
750 km
|
1000 km/h
|
turbojet
|
Surface
|
1984
|
1700 kg
|
410 kg conventional/200 kt nuclear
|
3000 km
|
828 km/h
|
turbofan
|
Air
|
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