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Natan Flayer · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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BAir defence
series of surface-to-air anti-ballistic missile and anti-aircraft defense systems
At a glance
Measured figures
Length
Single source2.1 m (6.9 ft)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Length
Single sourceConfiguration
| Specification | Barak 1 | Sky Bow |
|---|---|---|
| Type | SAM -based CIWS[source] | series of surface-to-air anti-ballistic missile and anti-aircraft defense systems[source] |
| Place of origin | Israel[source] | — |
| Manufacturer | Israel Aerospace Industries (IAI) & Rafael Advanced Defense Systems[source] | National Chung-Shan Institute of Science and Technology (NCSIST)[source] |
| Warhead | 22 kg (49 lb) blast fragmentation warhead[source] | — |
| Detonation mechanism | Proximity fuse |
Sky Bow II only; retired Sky Bow I values not inherited · Length
Single source5.673 m[source]Sky Bow II only; retired Sky Bow I values not inherited
5.498 m[source]Sky Bow III only; retired Sky Bow I values not inherited
Diameter
Single source170 mm (6.7 in)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Diameter
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Diameter
Single source0.42 m[source]Sky Bow II only; retired Sky Bow I values not inherited
0.4 m[source]Sky Bow III only; retired Sky Bow I values not inherited
Mass
Single source98 kg (216 lb)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Mass
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Mass
Single source1,135 kg[source]Sky Bow II only; retired Sky Bow I values not inherited
870 kg[source]Sky Bow III only; retired Sky Bow I values not inherited
Operational; Operational range
Single source0.5–12 km (0.3–7.5 mi)[source]
Sky Bow III only; retired Sky Bow I values not inherited · Range
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Range
Single source150 km[source]Sky Bow II only; retired Sky Bow I values not inherited
200 km[source]Sky Bow III only; retired Sky Bow I values not inherited
Sky Bow II only; retired Sky Bow I values not inherited · Warhead mass
Single source90 kg[source]Sky Bow II only; retired Sky Bow I values not inherited
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Flight altitude | 5.5 km (18,000 ft)[source] | — |
|---|
| Guidance system | Radar CLOS guidance[source] | — |
|---|
| Launch platform | Surface Ship[source] | Underground silos and mobile launch vehicles[source]Sky Bow II only; retired Sky Bow I values not inherited Towed quad launchers[source]Sky Bow III only; retired Sky Bow I values not inherited |
|---|
| Former operator · Venezuela | Venezuela[source] | — |
|---|
| In service | — | The TK-2, TK-3 and TK-4 are in service with the Military of the Republic of China[source] |
|---|
| Used by | — | Military of the Republic of China[source] |
|---|
| Role | — | surface-to-air missile[source]Sky Bow II only; retired Sky Bow I values not inherited surface-to-air missile[source]Sky Bow III only; retired Sky Bow I values not inherited |
|---|
| Propulsion | — | Single-stage dual-thrust solid-fuel rocket motor[source]Sky Bow II only; retired Sky Bow I values not inherited Solid-fuel rocket motor[source]Sky Bow III only; retired Sky Bow I values not inherited |
|---|
| Guidance | — | Inertial with mid-course guidance update from ground-based phased array radar, Active radar homing ( ARH ) for terminal guidance[source]Sky Bow II only; retired Sky Bow I values not inherited |
|---|
| Introduced | — | 1997[source]Sky Bow II only; retired Sky Bow I values not inherited |
|---|
| Country of origin | — | Taiwan[source]Inventory Origin column; table 5, row 4, cell 2; revision 1370505017; retrieved 2026-09-30 |
|---|
| Reported operators |
| — |
|---|