Comparison
| Name | Year | Weight | Warhead | Range | Speed (km/h) | Propulsion | launched by | Guidance | Built by | Comments |
| Fritz X | 1943 | kg | 320 kg | 5 km | 1235 km/h | none | Air | manual (radio link) | DE | used in combat |
| Henschel Hs 293 | 1943 | kg | 295 kg | 5.0 km | 828 km/h | Liquid-propellant, then gliding | Air | manual (radio link) | DE | used in combat |
| Kh-55 | 1984 | kg | 200 kt nuclear/410 kg conventional | 3000 km | 828 km/h | turbofan | Air | Inertial by Radar, TERCOM, Infrared | USSR/Russia | |
| Blohm & Voss BV 246 | 1943 | kg | 435 kg | 210 km | 450 km/h (280 mph) | none | Air | manual (radio link) | DE | |
| Ohka | 1943 | kg | 1200 kg | 36 km | 630 km/h | Solid-propellant | Air | human kamikaze | JP | used in combat |
| Bat | 1942 | kg | 273 kg | 37 km | 260–390 km/h | None | Air | manual (radio link) | USA | used in combat |
| Harpoon | 1977 | 691 kg | 221 kg | 280 km | 864 km/h | turbojet engine | Air, surface, sub | radar (B3: midcourse update) | USA | used in combat |
| AS.34 Kormoran | 1991 | 630 kg | 220 kg | 35 km | Mach 0.9 | rocket | Air | Inertial, active radar | DE | |
| Penguin | 1972 | 385 kg | 130 kg | 55+ km | high subsonic | Solid propellant | Air, surface, sub | Inertial, laser, IR | NOR | |
| AGM-65F Maverick | 1972 | 300 kg | 140 kg | 17 nm (30 km) | supersonic | Solid propellant | Air, | Laser, IR | USA | used in combat |
| Naval Strike Missile | 2009 | 410 kg | 125 kg | 185 km | high subsonic | turbojet and solid fuel booster | Air, surface | Inertial, GPS, terrain-reference, imaging IR, target database | NOR | |
| AGM-123 Skipper II | 1985 | 582 kg | 450 kg | 25 km | 1,100 km/h | solid-fueled | Air | laser-guided | USA | |
| SS.12/AS.12 | 1960 | kg | 28 kg | 7 km | 370 km/h | solid-fueled | Air, surface | wire MCLOS | FR | |
| BGM-109B Tomahawk | 1983 | 1.200 kg | 450 kg | 450 km | 880 km/h | turbofan | Air, surface, sub | GPS, TERCOM, DSMAC | USA | used in combat |
| Rb 04 | 1955 | kg | 300 kg | 32 km | subsonic | solid propellant | Air | active radar | SWE | |
| RB 08 | 1966 | kg | kg | 70 km | subsonic | turbojet | surface | radio link active radar | SWE | |
| RBS-15 | 1985 | 800 kg | 200 kg | 200 km | subsonic | turbojet | Air, surface | inertial, GPS, radar | SWE | |
| Exocet | 1979 | 670 kg | 165 kg | 180 km | 1134 km/h | solid propellant | Air, surface, sub | Inertial, active radar | FR | used in combat |
| Gabriel | 1962 | 522 kg | 150 kg | 60 km | 840 km/h | solid-fuel rocket | Air, surface | active radar | IL | used in combat |
| Otomat | 1977 | 770 kg | 210 kg | 180+ km | 1116 km/h | Turbojet | Surface,Air(Perú) | Inertial, GPS, active radar | IT | |
| Martel | 1984 | 550 kg | 150 kg | 60 km max | 1070 km/h | solid propellant | Air | passive radar, video | UK/FR | |
| Sea Eagle | 1985 | 580 kg | 230 kg | 110 km + | 1000 km/h | Turbojet | Air | Inertia, active radar | UK | |
| Sea Skua | 1983 | 145 kg | 28 kg | 25 km | 950 km/h | solid fuel | Air | semi-active radar | UK | used in combat |
| LRASM | 2013 | liquid fuel | Surface | USA | ||||||
| KSShch (SS-N-1 SCRUBBER) | 1958 | kg | nuclear | 40 km | 1150 km/h (Mach 0.95) | liquid-fuel rocket | Surface | inertial | USSR | |
| P-15 Termit (SS-N-2 STYX) | 1958 | kg | 454 kg | 80 km | 1100 km/h | Liquid fuel rocket | Surface | active radar, IR | USSR | used in combat |
| P-5 Pyatyorka (SS-N-3 SHADDOCK) | 1959 | kg | 1000 kg | 750 km | 1000 km/h | turbojet | Surface | Inertial, mid course correction, active radar | USSR | |
| Kh-22 (AS-4 Kitchen) | 1962 | kg | conventional/nuclear 1000 kg | 400 km | 4000 km/h | liquid-fuel rocket | Air | inertial | USSR | |
| P-70 Ametist (SS-N-7 STARBRIGHT) | 1968 | kg | 500 kg | 65 km | 1050 km/h | solid rocket | sub | inertial, terminal homing | USSR | |
| Moskit (SS-N-22 SUNBURN) | 1970 | 4.500 kg | 320 kg | 120 km | 3600 km/h | ramjet | Surface, Air | active radar, IR | USSR | |
| P-120 Malakhit (SS-N-9 SIREN) | 1972 | kg | 500 kg (1,100 lb) | 110 km | Mach 0.9 | Turbojet, solid fuel | Surface | Inertial, mid course correction, active radar | USSR | used in combat |
| P-800 Oniks (SS-N-26) | 1983 | 3.000 kg | 250 kg | 300 km | 3600 km/h | ramjet | Surface, Air | active-passive, radar | USSR | |
| 3M-54 Klub (SS-N-27 SIZZLER) | 1993 | 1.300-2.300 kg | 400 kg | 300 km | 735–3675 km/h | Turbojet | Surface, Sub | Inertial + Active Radar | USSR | |
| Kh-35 (AS-20 KAYAK) | 1983 | 520 kg | 145 kg | 130 km | 970 km/h | turbofan | Surface, Air | Inertial, active radar | USSR | |
| Kh-15 (AS-16 Kickback) | 1988 | 1.200 kg | 150 kg conventional/nuclear | 300 km | 6200 km/h | solid-fuel rocket | Air | inertial or active radar | USSR | |
| Hae Sung-I (SSM-700K) | 2005 | 718 kg | 300 kg | 150 km | 1013 km/h | Turbojet | Ship, Surface | Inertial, active radar | S.Korea | |
| SOM (missile) | 2006 | 600 kg | 230 kg | 185+ km | 1153 km/h | Turbojet | Air | INS / GPS, Terrain Referenced Navigation, Automatic Target Recognition, Imaging Infrared Seeker | Turkey | |
| BrahMos | 2006 | 2.500 kg (air), 3.000 kg (ground) | 300 kg | 290 km | 3675 km/h | ramjet | Ship,Surface, Air,Sub | Inertial, active radar | India/Russia |
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