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At a glance
Measured figures
Spike ER
Single sourceSpike MR/LR
Single sourceConfiguration
| Specification | Spike (missile) | TAipers |
|---|---|---|
| Type | Anti-tank guided missile[source] | Anti-tank guided missile[source] |
| Place of origin | Israel[source] | South Korea[source] |
| In service | 1981–present (Spike NLOS) 1997–present[source] | 2024–present[source] |
| Used by | See Operators (41 countries ordered it )[source] | Republic of Korea Army Republic of Korea Marine Corps |
Spike MR/LR : 1,200 mm (3 ft 11 in) Spike ER : 1,670 mm (5 ft 6 in)[source]
Launch pad
Single sourceMissile
Single sourceMissile: 1,735 millimeters (5 ft 8.3 in) Launch pad: 1,855 millimeters (6 ft 1.0 in)[source]
Battery
Single sourceCommand & Launch Unit
Single sourceLauncher
Single sourceLauncher + 4 Missiles · source measurement 4
Single sourceLauncher + 4 Missiles · source measurement 9
Single sourceLauncher + 4 Missiles Spike MR/LR from Tripod : Missile Round
Single sourceSpike ER from Helicopter : Missile Round
Single sourceThermal Sight Spike SR : Missile Round
Single sourceTripod
Single sourceSpike ER from Helicopter : Missile Round: 34 kg (75 lb) Launcher: 55 kg (121 lb) Launcher + 4 Missiles: 187 kg (412 lb) Spike MR/LR from Tripod : Missile Round: 14 kg (31 lb) Command & Launch Unit: 5 kg (11 lb) Tripod: 2.8 kg (6.2 lb) Battery: 1 kg (2.2 lb) Thermal Sight: 4 kg (8.8 lb) Spike SR : Missile Round: 9.6 kg (21 lb)[source]
Launch pad
Single sourceMissile
Single sourceMissile: 35 kilograms (77 lb) Launch pad: 9 kilograms (20 lb)
Maximum; Mach 0.59
Single sourceMaximum; Maximum speed · source measurement 1
Single sourceMaximum; Maximum speed · source measurement 2
Single source200 m/s (720 km/h; 450 mph; Mach 0.59)[source]
Effective; Air
Single sourceEffective; Spike ER
Single sourceEffective; Spike ER 2
Single sourceEffective; Spike ER 2 Spike NLOS : Land
Single sourceEffective; Spike LR
Single sourceEffective; Spike LR 2
Single sourceEffective; Spike MR
Single sourceEffective; Spike SR
Single sourceSpike SR : 50–1,500 m (55–1,640 yd) Spike MR : 200–2,500 m (220–2,730 yd) Spike LR : 200–4,000 m (220–4,370 yd) Spike LR 2 : 200–5,500 m (220–6,010 yd) Spike ER : 400–8,000 m (440–8,750 yd) Spike ER 2 : 400–10,000 m (440–10,940 yd) Spike NLOS : Land: 600–32,000 m (660–35,000 yd) Air: 600–50,000 m (660–54,680 yd)[source]
Effective; Effective firing range
Single sourceMaximum; Maximum firing range
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | 1982 Lebanon War Second Intifada Iraq War 2006 Lebanon War Afghanistan War 2008 Gaza War 2014 Gaza War 2016 Nagorno-Karabakh conflict Second Nagorno-Karabakh War 2023 Gaza War Twelve-Day War 2025 Cambodia-Thailand conflict[source] | — |
|---|
| Designer | Rafael Advanced Defense Systems[source] | Agency for Defense Development[source] |
|---|
| Designed | Late 1970s (Spike NLOS)[source] | 2015–2022[source] |
|---|
| Manufacturer | Rafael Advanced Defense Systems & EUROSPIKE GmbH Rafael Advanced Defense Systems Diehl Defence Rheinmetall Defence Electronics ST Engineering (Singapore)[source] | Hanwha Aerospace[source] |
|---|
| Unit cost | $249,966 (US Army Spike NLOS, 2022), $140,000 (German Spike LR, 2017)[source] | — |
|---|
| Produced | Spike NLOS : Since early 1980s Spike MR/LR/ER : Since 1997 Spike SR : Since 2012[source] | 2024–present[source] |
|---|
| No. built | 40,000 (2023) (7,000 fired)[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Rate of fire | Ready to launch: 30 s Time to reload: 15 s[source] | — |
|---|
| Sights | 10× Optical sight[source] | — |
|---|
| Warhead | HEAT Tandem-charge[source] | Tandem-charge HEAT[source] |
|---|
| Detonation mechanism | Piezoelectric trigger[source] | — |
|---|
| Engine | Solid-propellant rocket[source] | — |
|---|
| Guidance system | Target Acquisition : Infrared seeker CCD Missile Guidance: IIR homing CCD CCD + IIR[source] | Fire-and-forget dual-mode seeker with fiber-optic datalink MITL[source] |
|---|
| Blast yield | — | 1,000 mm (39 in) RHA[source] |
|---|
| Propellant | — | Smokeless solid-propellant[source] |
|---|
| Launch platform | — | LAH-1 Miron MAH Marineon[source] |
|---|