FORCETALLY
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At a glance
Measured figures
Length
Single source1200 mm[source]
UMTAS-GM-2
Single sourceConfiguration
| Specification | 9M133 Kornet | UMTAS |
|---|---|---|
| Type | Anti-tank missile[source] | Air-to-surface , anti-tank guided missile[source] |
| Place of origin | Russia[source] | Turkey[source] |
| In service | 1998–present[source] | — |
| Used by | See Operators[source] | — |
| Wars | Iraq War 2006 Lebanon War Israeli–Palestinian conflict 2021 Israel–Palestine crisis Gaza war Libyan Crisis (2011–present) Syrian Civil War War in Iraq (2013–2017) Russo-Ukrainian War Russo-Ukrainian war (2022–present) Yemeni Civil War Saudi Arabian-led intervention in Yemen Sinai insurgency 2020 Nagorno-Karabakh conflict |
UMTAS/LUMTAS
Single sourceUMTAS/LUMTAS-GM-1
Single sourceUMTAS/LUMTAS -1.8 m (5 ft 11 in) UMTAS/LUMTAS-GM-1 -1.72 m (5 ft 8 in) UMTAS-GM-2 -2 m (6 ft 7 in)[source]
Mass
Single sourceweight with tripod/firing unit
Single sourcewith launch tube) /
Single source27 kg (29 kg with launch tube) / 63.7 kg (weight with tripod/firing unit)[source]
UMTAS-GM-2 launcher
Single sourceUMTAS-GM-2 missile
Single sourceOperational; anti-tank
Single sourceOperational; high explosive
Single sourceOperational; Kornet Kornet-EM
Single sourceKornet 100–5,500 m Kornet-EM 8,000 m (anti-tank), 10,000 m (high explosive)[source]
Operational; UMTAS-GM-2 from aircraft
Single sourceOperational; UMTAS-GM-2 from vehicles
Single sourceHEAT
Single source4.6 kg (10 lb) HEAT[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designer | KBP Instrument Design Bureau[source] | — |
|---|
| Designed | 1988–1998[source] | 2005-2017[source] |
|---|
| Manufacturer | Degtyarev plant[source] | Roketsan[source] |
|---|
| Unit cost | $26,000 per missile (2019, export cost)[source] | — |
|---|
| Produced | 1994–present[source] | 2017-current[source] |
|---|
| No. built | 35,000 (2009)[source] | — |
|---|
| Variants | See Variants[source] | UMTAS L-UMTAS[source] |
|---|
| Warhead | 1,000+ (9K135), 1,200+ (E), 1,300+ (D) mm RHA penetration after ERA with Tandem HEAT , Thermobaric[source] | Tandem HEAT / blast-fragmentation / thermobaric[source] |
|---|
| Detonation mechanism | Impact fuze[source] | Impact Proximity[source] |
|---|
| Propellant | Solid-fuel rocket[source] | — |
|---|
| Guidance system | SACLOS laser beam riding[source] | RF data link Imaging infrared (UMTAS) Semi-active laser (L-UMTAS)[source] |
|---|
| Steering system | Two control surfaces[source] | — |
|---|
| Accuracy | <5 m[source] | — |
|---|
| Launch platform | Individual, vehicles, Kornet-T , Kornet-D , Bumerang-BM , Kornet-D1 , Pokpung-Ho IV[source] | AH-1W SuperCobra T129 ATAK SH-60B Seahawk TAI Hürkuş TAI Hürjet IOMAX Archangel Mil Mi-8[source] |
|---|
| Engine | — | HTPB ‐based solid-fuel rocket motor[source] |
|---|
| References | — | Janes[source] |
|---|
| Reported operators |
| — |
|---|
UMTAS/LUMTAS-GM-1 launcher
Single sourceUMTAS/LUMTAS-GM-1 missile
Single sourceUMTAS/LUMTAS launcher
Single sourceUMTAS/LUMTAS missile
Single sourceUMTAS/LUMTAS -37.5 kg (83 lb) missile 62 kg (137 lb) launcher UMTAS/LUMTAS-GM-1 -41.3 kg (91 lb) missile 25 kg (55 lb) launcher UMTAS-GM-2 -60 kg (130 lb) missile 40 kg (88 lb) launcher[source]
Operational; UMTAS/LUMTAS
Single sourceOperational; UMTAS/LUMTAS-GM-1 from aircraft
Single sourceOperational; UMTAS/LUMTAS-GM-1 from vehicles
Single sourceUMTAS/LUMTAS -500–8,000 m (0.31–4.97 mi) UMTAS/LUMTAS-GM-1 -1,000–16,000 m (0.62–9.94 mi) from vehicles, 1,000–32,000 m (0.62–19.88 mi) from aircraft UMTAS-GM-2 -1,000–32,000 m (0.62–19.88 mi) from vehicles 1,000–50,000 m (0.62–31.07 mi) from aircraft[source]