FORCETALLY
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Measured figures
Operational; SAMAR I
Single sourceOperational; SAMAR II
Single sourceConfiguration
| Specification | SAMAR Air Defence System | Sevom Khordad |
|---|---|---|
| Speed | SAMAR I : Mach 2 to 2.5 SAMAR II : Mach 4.5[source] | — |
| Type | Surface-to-air missile[source] | Aerial defense system[source] |
| Place of origin | India[source] | Iran[source] |
| In service | 2022 ( 2022 )[source] | 2016–present |
SAMAR I : 10–12 km (6.2–7.5 mi) SAMAR II : 20 km (12 mi)[source]
Operational; Operational range
Single source50–200 km[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by | Indian Air force[source] | See § Operators[source] |
|---|
| Wars | India-Pakistan Conflict 2025[source] | 2019–2020 Persian Gulf crisis Twelve-Day War 2026 Iran War[source] |
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| Designer | 11 Base Repair Depot Ojhar with industry partner Adtech Inventions Pvt Ltd 7 Base Repair Depot Tughlakabad with industry partner Simran Flowtech Industries and Yamazuki Denki[source] | — |
|---|
| Variants | SAMAR I : Vympel R-73 SAMAR II : Vympel R-27[source] | — |
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| Detonation mechanism | Proximity fuze , contact fuze[source] | — |
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| Engine | Solid-propellant rocket[source] | IVECO diesel[source] |
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| Propellant | Solid fuel[source] | — |
|---|
| Guidance system | SAMAR I : Infrared homing SAMAR II : Semi-active radar homing , infrared homing[source] | — |
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| Launch platform | SAMAR I : Ashok Leyland Stallion SAMAR II : BEML - Tatra T815 8WD[source] | — |
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| Main armament | — | Taer-2B[source] |
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| Secondary armament | — | Sayyad-2[source] |
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| Flight altitude | — | 25–30 km[source] |
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| Reported operators | — |
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