Credit
Rama · CC BY-SA 2.0 fr · Resized · CC BY-SA 2.0 fr · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
MILANlarger figure on 0 of 6
Nag (missile)larger figure on 6 of 6
Measured figures
Length
Single source1.2 m (3 ft 11 in)[source]
Length
Single sourceConfiguration
| Specification | MILAN | Nag (missile) |
|---|---|---|
| Type | Anti-tank missile[source] | Anti-tank guided missile[source] |
| Place of origin | France, West Germany[source] | India[source] |
| In service | 1972–present[source] | 2019 ( 2019 ) –present[source] |
| Used by | See operators[source] | Indian Army Indian Air Force[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
1.83 m (6 ft 0 in)[source]
Operational; Operational range
Single sourceOperational; MILAN ER
Single source200–2,000 m (660–6,560 ft); 3,000 m (MILAN ER)[source]
Operational; Operational range
Single sourceOperational; HELINA/Dhruvastra
Single sourceWarhead weight
Single source8 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | South African Border War Chadian-Libyan conflict Toyota War Western Sahara War Lebanese Civil War Iran–Iraq War Falklands War Gulf War 2003 invasion of Iraq Iraq War Opération Licorne Libyan Civil War Northern Mali Conflict Operation Sangaris War in Iraq (2013–2017) Syrian Civil War Russian invasion of Ukraine[source] | — |
|---|
| Designed | 1970s[source] | — |
|---|
| Manufacturer | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] | Bharat Dynamics Limited[source] |
|---|
| Unit cost | £7,500 (1984)[source] | ₹ 1 crore (US$100,000)[source] |
|---|
| Produced | 1971[source] | — |
|---|
| No. built | 350,000 missiles, 10,000 launchers[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | Single or tandem HEAT[source] | Tandem-charge HEAT (Penetration >900 mm in ERA + RHA )[source] |
|---|
| Detonation mechanism | contact[source] | — |
|---|
| Engine | solid-fuel rocket[source] | Solid-propellant rocket booster and sustainer motor[source] |
|---|
| Guidance system | SACLOS wire[source] | Mid-course: CCD + area correlation + two-way datalink Terminal: IIR homing (HELINA/Dhruvastra) MMW ARH (SANT)[source] |
|---|
| Steering system | Jet deflector[source] | — |
|---|
| Launch platform | Individual, vehicle[source] | NAMICA HAL Rudra HAL Prachand Mil Mi-24 Zorawar LT[source] |
|---|
| Designer | — | Defence Research and Development Organisation[source] |
|---|
| Propellant | — | Nitramine smokeless extruded double base[source] |
|---|
| Alternative designation | — | Prospina[source] |
|---|
| Reported operators |
| — |
|---|
Operational; Nag (ProspiNa)
Single sourceOperational; SANT
Single sourceNag (ProspiNa): 500m–4km HELINA/Dhruvastra: 7–10km SANT: 15–20km[source]