Credit
Mztourist · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
CAIG Wing Loong IIlarger figure on 0 of 1
Palianytsia (missile)larger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | CAIG Wing Loong II | Palianytsia (missile) |
|---|---|---|
| Crew | None[source] | — |
| Type | MALE UCAV[source] | Turbojet drone[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Ukroboronprom[source] |
| Designer | Chengdu Aircraft Design Institute[source] | Luch Design Bureau[source] |
| Status |
Wingspan
Single source20.5 m (67 ft 3 in)[source]
Operational; Operational range
Single source650 km[source]
Service ceiling
Single source9,900 m (32,500 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| — |
| Primary user | People's Liberation Army Air Force Pakistan Air Force[source] | — |
|---|
| Manufactured | 2015-present[source] | — |
|---|
| Introduction date | 2017[source] | — |
|---|
| First flight | February 2017[source] | — |
|---|
| Developed from | CAIG Wing Loong[source] | — |
|---|
| Developed into | Chengdu Wing Loong-3[source] | — |
|---|
| Stall speed | 150 km/h (93 mph, 81 kn)[source] | — |
|---|
| Country of origin | China[source]Inventory Origin column; table 3, row 4, cell 2; revision 1375623248 | — |
|---|
| Origin reported by inventory | People's Republic of China[source]Inventory Origin column; table 3, row 27, cell 2; revision 1347318478 | — |
|---|
| Place of origin | — | Ukraine[source] |
|---|
| In service | — | 2024[source] |
|---|
| Used by | — | Ukraine[source] |
|---|
| Wars | — | Russo-Ukrainian War[source] |
|---|
| Produced | — | 2024[source] |
|---|
| Engine | — | turbojet[source] |
|---|
| Flight altitude | — | 15–500 m[source] |
|---|
| Guidance system | — | INS, GPS[source] |
|---|
| Reported operators |
| — |
|---|