Credit
Baiweiflight · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Wing Loong I · Length
Single source9.05 m (29 ft 8 in)[source]
Length
Single sourceConfiguration
| Specification | CAIG Wing Loong | Pegaz |
|---|---|---|
| Crew | None (UAV)[source] | — |
| Type | MALE UCAV[source] | Unmanned combat aerial vehicle[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Utva Aviation Industry[source] |
| Designer | Chengdu Aircraft Design Institute[source] | Military Technical Institute[source] |
| Status | in service & in production |
5.395 m (17 ft 8 in)[source]
Wing Loong I · 1 × Rotax 914 turbocharged 100 shp
Single source1 × Rotax 914 turbocharged, 75 kW (100 shp)[source]
Wing Loong I · of air-to-surface weapons
Single source200 kilograms (440 lb) of air-to-surface weapons[source]
Wing area
Single source4.24 m 2 (45.6 sq 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 users | People's Liberation Army Air Force Egyptian Air Force United Arab Emirates Air Force Pakistan Air Force[source] | — |
|---|
| Manufactured | 2009[source] | 2011–present[source] |
|---|
| Introduction date | 2011[source] | 2025[source] |
|---|
| First flight | 2009[source] | 2011[source] |
|---|
| Developed into | CAIG Wing Loong II[source] | — |
|---|
| Propellers | 3-bladed[source] | 2-bladed pusher propeller[source] |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| National origin | — | Serbia[source] |
|---|
| Primary user | — | Serbian Air Force and Air Defence[source] |
|---|
| Number built | — | 12+[source] |
|---|
| Capacity | — | 50 kg (110 lb) payload[source] |
|---|
| Rockets | — | 2 × FT-8D laser guided rocket[source] |
|---|
| Reported operators |
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