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BAir defence
series of surface-to-air anti-ballistic missile and anti-aircraft defense systems
At a glance
Measured figures
Shalamche
Single sourceShalamche : 5,030 mm[source]
Sky Bow III only; retired Sky Bow I values not inherited · Length
Single sourceConfiguration
| Specification | Mersad | Sky Bow |
|---|---|---|
| Speed | More than Mach 2.4, Shalamche : Mach 3[source] | Mach 4.5[source]Sky Bow II only; retired Sky Bow I values not inherited Mach 7.0[source]Sky Bow III only; retired Sky Bow I values not inherited |
| Type | Air defense system[source] | series of surface-to-air anti-ballistic missile and anti-aircraft defense systems[source] |
| Place of origin | Iran[source] | — |
| In service | 2010–present[source] |
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
Shalamche
Single sourceShalamche : 356 mm[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
Shalamche
Single sourceShalamche : 636 kg[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; Planned
Single sourceOperational; Shahin
Single sourceOperational; Shalamche Phase II : ~
Single sourceShahin : 45 km (30 miles) Shalamche : 40 km Phase II : ~60 km (Planned)[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 sourceSky 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.
The TK-2, TK-3 and TK-4 are in service with the Military of the Republic of China[source] |
| Used by | Iran Syria Maldives[source] | Military of the Republic of China[source] |
|---|
| Produced | Since 2010[source] | — |
|---|
| Variants | Mersad, Mersad Phase I, Mersad Phase II (Under Development)[source] | — |
|---|
| Main armament | 3× Shahin or Shlamche missiles[source] | — |
|---|
| Engine | Solid propellant rocket engine[source] | — |
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| Guidance system | Semi-active radar homing[source] | — |
|---|
| Manufacturer | — | National Chung-Shan Institute of Science and Technology (NCSIST)[source] |
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| 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 |
|---|
| Launch platform | — | 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 |
|---|
| 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 |
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| Introduced | — | 1997[source]Sky Bow II only; retired Sky Bow I values not inherited |
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| Country of origin | — | Taiwan[source]Inventory Origin column; table 5, row 4, cell 2; revision 1370505017; retrieved 2026-09-30 |
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| Reported operators |
| — |
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