FORCETALLY
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At a glance
Measured figures
AR-1 specification-table column only, not AR-2 · Length
Single source1,400 mm (4.6 ft)[source]AR-1 specification-table column only, not AR-2
Configuration
| Specification | AR-1 (missile) | Zuni (rocket) |
|---|---|---|
| Type | air-to-ground anti-tank missile[source] | Air-to-surface rocket[source] |
| National origin | Chinese[source] | — |
| Designer | 11th Academy of the China Aerospace Science and Technology Corporation (CASC)[source] | — |
| Launch platforms | unmanned aerial vehicles (UAVs), helicopters, and fixed-wing aircraft[source] | — |
| Guidance | inertial navigation system and semi-active laser homing[source] |
Length
77 inches (2,000 mm)[source]
AR-1 specification-table column only, not AR-2 · Wingspan
Single source370 mm (15 in)[source]AR-1 specification-table column only, not AR-2
AR-1 prose reported launch mass · around
Single sourceLaunch; AR-1 specification-table column only, not AR-2 · Launch mass
Single sourcearound 40 kg (88 lb)[source]AR-1 prose reported launch mass
42 kg (93 lb)[source]AR-1 specification-table column only, not AR-2
motor only
Single source79.5 pounds (36.1 kg) (motor only)[source]
AR-1 specification-table column only, not AR-2 · Warhead mass
Single source9 kg (20 lb)[source]AR-1 specification-table column only, not AR-2
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
INS (LOBL/LOAL) + SAL / infrared homing / Television (TV) / mmW radar[source]AR-1 specification-table column only, not AR-2
| — |
| Seeker configuration | The seeker head is modular and can be replaced with other types.[source] | — |
|---|
| Release altitude | 500–5,000 m (1,600–16,400 ft)[source]AR-1 specification-table column only, not AR-2 | — |
|---|
| Release speed | 180–250 km/h (97–135 kn)[source]AR-1 specification-table column only, not AR-2 | — |
|---|
| Warhead type | Penetration blast warhead / Fragmentation-blast warhead[source]AR-1 specification-table column only, not AR-2 | — |
|---|
| Steering | Double cruciform trailing edges (X-X)[source]AR-1 specification-table column only, not AR-2 | — |
|---|
| Accuracy | ≤1.5m[source]AR-1 specification-table column only, not AR-2 | — |
|---|
| Place of origin | — | United States[source] |
|---|
| Used by | — | United States military French Air Force Ukrainian Air Force[source] |
|---|
| Produced | — | 1957–present[source] |
|---|
| Warhead | — | various[source] |
|---|
| Engine | — | Solid-fuel rocket[source] |
|---|
| Guidance system | — | None[source] |
|---|