Credit
Baiweiflight · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Wing Loong I · Length
Single source9.05 m (29 ft 8 in)[source]
Configuration
| Specification | CAIG Wing Loong | Lihiniya MK I |
|---|---|---|
| Crew | None (UAV)[source] | — |
| Type | MALE UCAV[source] | Unmanned aerial vehicle[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Sri Lanka Air Force Centre for Research and Development[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
| Status | in service & in production[source] |
Wing Loong I · Wingspan
Single source14 m (45 ft 11 in)[source]
Wing Loong I · Height
Single source2.77 m (9 ft 1 in)[source]
Wing Loong I · of air-to-surface weapons
Single source200 kilograms (440 lb) of air-to-surface weapons[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Primary users | People's Liberation Army Air Force Egyptian Air Force United Arab Emirates Air Force Pakistan Air Force[source] | — |
|---|
| Manufactured | 2009[source] | — |
|---|
| Introduction date | 2011[source] | — |
|---|
| First flight | 2009[source] | — |
|---|
| Developed into | CAIG Wing Loong II[source] | Lihiniya MK II[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| National origin | — | Sri Lanka[source] |
|---|
| Primary user | — | Sri Lanka Air Force[source] |
|---|
| Fuel capacity | — | 19 liter[source] |
|---|
| Reported operators |
| — |
|---|