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 | Schiebel Camcopter S-100 |
|---|---|---|
| Crew | None (UAV)[source] | None[source] |
| Type | MALE UCAV[source] | UAV[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Schiebel , Austria[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
| Status |
3.11 m (10 ft 2 in)[source]
Wing Loong I · Wingspan
Single source14 m (45 ft 11 in)[source]
Main rotor diameter
Single source3.4 m (11 ft 2 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.
in service & in production[source] |
in service[source] |
| Primary users | People's Liberation Army Air Force Egyptian Air Force United Arab Emirates Air Force Pakistan Air Force[source] | French Navy Royal Navy United States Navy[source] |
|---|
| Manufactured | 2009[source] | — |
|---|
| Introduction date | 2011[source] | 2005[source] |
|---|
| First flight | 2009[source] | — |
|---|
| Developed into | CAIG Wing Loong II[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| Number built | — | > 540[source] |
|---|
| Capacity | — | 50 kg (110 lb)[source] |
|---|
| Fuel capacity | — | 57 L (15.5 gal) AVGas 100 LL[source] |
|---|
| Hardpoints | — |
|---|
| Never exceed speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| g limits | — | +3.5 g to –1 g[source] |
|---|
| Missiles | — | 2x Lightweight Multirole Missile[source] |
|---|
| National origin | — | Austria[source] |
|---|
| Alternative designation | — | Camcopter S-100[source] |
|---|
| Reported operators |
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