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Mztourist · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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BDrones & UAVs
Unmanned surveillance and reconnaissance aerial vehicle and Unmanned combat aerial vehicle (armed variant)
At a glance
CAIG Wing Loong IIlarger figure on 4 of 4
Measured figures
Length
Single source11 m (36 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | CAIG Wing Loong II | HESA Hamaseh |
|---|---|---|
| Crew | None[source] | — |
| Type | MALE UCAV[source] | Unmanned surveillance and reconnaissance aerial vehicle and Unmanned combat aerial vehicle (armed variant)[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Iran Aircraft Manufacturing Industrial Company (HESA)[source] |
| Designer | Chengdu Aircraft Design Institute[source] | HESA[source] |
HESA Hamasehlarger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
5.05 m (16 ft 7 in)[source]
Combat range
Single source200 km (120 mi, 110 nmi)[source]
790 ft/min
Single source4 m/s (790 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In service[source] |
|---|
| Primary user | People's Liberation Army Air Force Pakistan Air Force[source] | Iranian Armed Forces[source] |
|---|
| Manufactured | 2015-present[source] | 2013–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] | 110 km/h (68 mph, 59 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 | — | Iran[source] |
|---|
| Number built | — | 30 (2013)[source] |
|---|
| Source measurement | — | The Hamaseh can carry up to 185 kg of fuel, equipment, and payload, and has an endurance of up to 11 hours depending on configuration. It is launched via runway takeoff or JATO , and is recovered by runway landing or, in emergencies, a parachute. The Hamaseh can follow pre-determined waypoints to control its flight. Its powerplant is unknown.[source]HESA Hamaseh · Design; only the objects and conditions stated in this passage Length: 5.05 m (16 ft 7 in)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Width: 9 m (29 ft 6 in)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Height: 1.9 m (6 ft 3 in)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Empty weight: 230 kg (507 lb)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Gross weight: 415 kg (915 lb)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Maximum speed: 194 km/h (121 mph, 105 kn)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Cruise speed: 165 km/h (103 mph, 89 kn)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Stall speed: 110 km/h (68 mph, 59 kn)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Combat range: 200 km (120 mi, 110 nmi)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Endurance: up to 11 h (depending on payload)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Service ceiling: 4,600 m (15,000 ft)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage Rate of climb: 4 m/s (790 ft/min)[source]HESA Hamaseh · Specifications; only the objects and conditions stated in this passage |
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| Reported operators |
| — |
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