

Preparing your view.


At a glance
Measured figures
Wing Loong I · Wingspan
Single source14 m (45 ft 11 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]
Falcon 8+ · 1,936 ft/min (
Single source1,936 ft/min (10 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | CAIG Wing Loong | Intel Falcon 8 |
|---|---|---|
| Width | — | 2,680 ft 5 in (817 m)[source]Source text · numeric interpretation needs review |
| Crew | None (UAV)[source] | — |
| Type | MALE UCAV[source] | Camera drone[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Ascending Technologies (later Intel )[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
| Status | in service & in production[source] | — |
| Primary users | People's Liberation Army Air Force Egyptian Air Force United Arab Emirates Air Force Pakistan Air Force[source] | — |
| Manufactured | 2009[source] | 2009–present[source] |
| Introduction date | 2011[source] | 2009[source] |
| First flight | 2009[source] | — |
| Developed into | CAIG Wing Loong II[source] | — |
| Propellers | 3-bladed[source] | 2-bladed, 8.0 in (0.2032 m) diameter[source] |
| Country of origin | People's Republic of China[source] | — |
| National origin | — | Germany/United States[source] |
| Capacity | — | 1.76 lb (0.8 kg) payload[source] |
| Battery | — | 2× Intel Powerpack 4000[source] |
| Powerplant | — | 8 × 125W brushless DC electric motor[source] |
| Maximum wind resistance | — | 35.8 miles per hour (57.6 km/h)[source] |
| Operating temperature | — | 23°F (-5°C) to 113°F (45°C)[source] |
| GNSS compatibility | — | GPS , GLONASS[source] |
| Reported operators |
| — |