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At a glance
Type 79 Jyu-MATlarger figure on 1 of 3
Zuni (rocket)larger figure on 2 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source1.5 m[source]
Length
Single sourceConfiguration
| Specification | Type 79 Jyu-MAT | Zuni (rocket) |
|---|---|---|
| Type | Heavy anti-tank/landing-craft guided missile[source] | Air-to-surface rocket[source] |
| Place of origin | Japan[source] | United States[source] |
| In service | 1984 to present[source] | — |
| Used by | Japan[source] | United States military French Air Force Ukrainian Air Force[source] |
77 inches (2,000 mm)[source]
Operational; Operational range
Single source5 miles (8.0 km)[source]
Warhead weight
Single source4.2 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
Defense Agency Technical Research and Development Institute[source] |
| — |
| Manufacturer | Kawasaki Heavy Industries[source] | — |
|---|
| Produced | 1980 to present[source] | 1957–present[source] |
|---|
| Warhead | Shaped charge on tanks/armored vehicles Fragmentation charged warhead for landing vessels and ships.[source] | various[source] |
|---|
| Detonation mechanism | Impact or delayed impact[source] | — |
|---|
| Guidance system | Wire guided SACLOS[source] | None[source] |
|---|
| Engine | — | Solid-fuel rocket[source] |
|---|