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BAir defence
series of surface-to-air anti-ballistic missile and anti-aircraft defense systems
Measured figures
Sky Bow III only; retired Sky Bow I values not inherited · Length
Single sourceSky Bow II only; retired Sky Bow I values not inherited · Length
Single sourceConfiguration
| Specification | PSR-A Pilica | Sky Bow |
|---|---|---|
| Speed | — | 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 | Anti-Aircraft System[source] | series of surface-to-air anti-ballistic missile and anti-aircraft defense systems[source] |
| Place of origin | Poland[source] | — |
| In service | 2020 – present[source] | The TK-2, TK-3 and TK-4 are in service with the Military of the Republic of China |
5.673 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
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
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; for
Single sourceOperational; for Grom/Piorun missiles
Single source6,500 m for Grom/Piorun missiles, 3,000m for 23 mm auto cannon[source]Source text · numeric interpretation needs review
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.
| Used by | Polish Air Force[source] | Military of the Republic of China[source] |
|---|
| Designed | 2015[source] | — |
|---|
| Manufacturer | Zakłady Mechaniczne Tarnów[source] | National Chung-Shan Institute of Science and Technology (NCSIST)[source] |
|---|
| Produced | 2019 – present[source] | — |
|---|
| Main armament | 2 Grom or Piorun missiles in the special starting rail, twin barrel 23 mm autocanon[source] | — |
|---|
| Suspension | Jelcz 442.32 4 x 4[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 |
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| 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 |
|---|
| 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 |
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