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At a glance
Measured figures
detachable CLU
Single sourceJavelin · missile and command launch unit together · Mass
Single sourcemissile in launch tube
Single sourceready to fire
Single source22.3 kg (49 lb), ready to fire 6.4 kg (14 lb), detachable CLU 15.9 kg (35 lb), missile in launch tube[source]
49.5 pounds[source]Javelin · missile and command launch unit together
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]
Effective; From vehicle
Single sourceEffective; Lightweight CLU
Single sourceEffective; Original CLU
Single sourceOriginal CLU: 2,500 m (1.6 mi) Lightweight CLU: 4,000 m (2.5 mi) From vehicle: 4,750 m (2.95 mi)[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]
Barrel length
Single source1.2 m (47 in)[source]
Warhead weight
Single source8.4 kg (19 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | FGM-148 Javelin | Spike (missile) |
|---|---|---|
| Crew | 1 or 2[source] | — |
| Type | Anti-tank missile Surface-to-surface missile Surface-to-air missile[source] | Anti-tank guided missile[source] |
| Place of origin | United States[source] | Israel[source] |
| In service | 1996–present[source] | 1981–present (Spike NLOS) 1997–present[source] |
| Used by | See Operators[source] | See Operators (41 countries ordered it )[source] |
| Wars | War in Afghanistan Iraq War Syrian Civil War Second Libyan Civil War Russo-Ukrainian War[source] | 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 | Texas Instruments & Martin Marietta , now Raytheon Technologies & Lockheed Martin[source] | Rafael Advanced Defense Systems[source] |
| Designed | June 1989[source] | Late 1970s (Spike NLOS)[source] |
| Manufacturer | Raytheon & Lockheed Martin[source] | Rafael Advanced Defense Systems & EUROSPIKE GmbH Rafael Advanced Defense Systems Diehl Defence Rheinmetall Defence Electronics ST Engineering (Singapore)[source] |
| Unit cost | US$216,717 (G-model missile only, FY2021) US$240,000 (missile only, export cost, FY2019) US$249,700 (Lightweight CLU only, FY2021)[source] | $249,966 (US Army Spike NLOS, 2022), $140,000 (German Spike LR, 2017)[source] |
| Produced | 1996–present[source] | Spike NLOS : Since early 1980s Spike MR/LR/ER : Since 1997 Spike SR : Since 2012[source] |
| No. built | 50,000 missiles (12,000 CLUs)[source] | 40,000 (2023) (7,000 fired)[source] |
| Variants | See: § Variants[source] | See variants[source] |
| Sights | Optical sight & thermal imaging[source] | 10× Optical sight[source] |
| Warhead | Tandem-charge HEAT[source] | HEAT Tandem-charge[source] |
| Detonation mechanism | Contact fuze[source] | Piezoelectric trigger[source] |
| Blast yield | Penetration: Stated as being in excess of 30 in (760 mm) RHA[source] | — |
| Propellant | Solid-fuel[source] | — |
| Flight ceiling | 150 m (490 ft) (top attack mode) 60 m (200 ft) (direct attack mode)[source] | — |
| Guidance system | Infrared homing[source] | Target Acquisition : Infrared seeker CCD Missile Guidance: IIR homing CCD CCD + IIR[source] |
| Launch platform | Man-portable launcher[source] | — |
| Launch platforms | shoulder-fired[source]Javelin | — |
| Rate of fire | — | Ready to launch: 30 s Time to reload: 15 s[source] |
| Engine | — | Solid-propellant rocket[source] |
| Reported operators |
| — |