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At a glance
Measured figures
Length
Single source12.2 m (40 ft 0 in)[source]
Mohajer-2 · Length
Single sourceConfiguration
| Specification | Hongdu GJ-11 | Qods Mohajer |
|---|---|---|
| Crew | None[source] | none[source] |
| Type | Unmanned combat aerial vehicle Loyal wingman drone[source] | Light/medium intelligence, surveillance, and reconnaissance (ISR)[source] |
| National origin | People's Republic of China[source] | Iran[source] |
| Manufacturer | Hongdu Aviation Industry Group[source] | Qods Aviation Industry Company , Tehran |
2.91 m (9 ft 7 in)[source]
Maximum; Mohajer-2 · Maximum speed
Single source200 km/h (120 mph, 110 kn)[source]
Mohajer-2 · Range
Single source50 km (31 mi, 27 nmi)[source]
Mohajer-2 · 1 × WAE-342 twin-cylinder piston engine
Single source1 × WAE-342 twin-cylinder piston engine, 19 kW (25 hp)[source]
Mohajer-2 · Endurance
Single source1.5h[source]
Mohajer-2 · Service ceiling
Single source3,350 m (10,990 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Shenyang Aircraft Design Institute Hongdu Aviation Industry Group Aviation Industry Corporation of China[source] | Qods Aviation Industry Company[source] |
|---|
| Status | In development[source] | In service[source] |
|---|
| Primary user | People's Liberation Army Air Force[source] | — |
|---|
| First flight | November 2013[source] | 1985[source] |
|---|
| Powerplant | 1 × unnamed Guizhou -built turbofan[source] | — |
|---|
| Primary users | — | Iran Syria Venezuela Hezbollah[source] |
|---|
| Number built | — | 253 (mid-2000s)[source] |
|---|
| Manufactured | — | 1980s–present[source] |
|---|
| Introduction date | — | February 1986[source] |
|---|
| Capacity | — | 15 kg payload[source] |
|---|
| Propellers | — | 2-bladed[source] |
|---|
| Reported operators | — |
|
|---|