Credit
玄史生 · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Hsiung Feng IIlarger figure on 2 of 3
Zuni (rocket)larger figure on 1 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source4,800 mm (190 in)[source]
Length
Single sourceConfiguration
| Specification | Hsiung Feng II | Zuni (rocket) |
|---|---|---|
| Type | Surface-to-surface missile[source] | Air-to-surface rocket[source] |
| Place of origin | Taiwan[source] | United States[source] |
| In service | Early 1990s-present[source] | — |
| Used by | Republic of China Armed Forces[source] | United States military French Air Force Ukrainian Air Force[source] |
77 inches (2,000 mm)[source]
Warhead weight
Single source180 kg (400 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | National Chung-Shan Institute of Science and Technology[source] | — |
|---|
| Variants | Air launched version without first stage rocket booster[source] | — |
|---|
| Guidance system | Inertial guidance midflight, terminal with dual active radar homing and infrared homing seekers[source] | None[source] |
|---|
| Launch platform | Box launcher or aircraft[source] | — |
|---|
| Produced | — | 1957–present[source] |
|---|
| Warhead | — | various[source] |
|---|
| Engine | — | Solid-fuel rocket[source] |
|---|