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 4 of 4
STC Orlan-10larger figure on 0 of 4
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 | STC Orlan-10 |
|---|---|---|
| Crew | None[source] | — |
| Type | MALE UCAV[source] | Reconnaissance unmanned aerial vehicle[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Special Technology Center (STC)[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
| Status | In service[source] |
Ferry; Ferry range
Single source600 km (370 mi, 320 nmi)[source]
Combat range
Single source110 km (68 mi, 59 nmi)[source]
1 × Saito Manufacturing FA-62B single-cylinder four-stroke glow fuel piston engine
Single source1 × Saito Manufacturing FA-62B single-cylinder four-stroke glow fuel piston engine , 0.71 kW (0.95 hp)[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 | — |
|---|
| National origin | — | Russia[source] |
|---|
| Primary users | — | Russian Ground Forces Ministry of Emergency Situations[source] |
|---|
| Capacity | — | 6 kg (13 lb) payload[source] |
|---|
| Launch method | — | folding catapult platform[source] |
|---|
| Landing method | — | parachute recovery[source] |
|---|
| Max. wind speed at launch | — | 10 m/s[source] |
|---|
| Operational temperature range | — | −30 to +40 °C[source] |
|---|
| Optical imaging | — | Canon EOS 750D / EOS 800D digital SLR camera with EF 85mm f/1.8 USM lens[source] |
|---|
| Thermal imaging | — | TM2005016-F19 Lynred PICO640gen2 infrared camera[source] |
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| Reported operators |
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