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Measured figures
Mohajer-2 · Length
Single source2.91 m (9 ft 7 in)[source]
Configuration
| Specification | Prioria Robotics Maveric | Qods Mohajer |
|---|---|---|
| Crew | — | none[source] |
| Type | Tactical, Squad-level, Hand-launched[source] | Light/medium intelligence, surveillance, and reconnaissance (ISR)[source] |
| Manufacturer | Prioria Robotics, Inc.[source] | Qods Aviation Industry Company , Tehran[source] |
| Production status | is a discontinued unmanned aerial vehicle[source]Ownproductiondiscontinuation; notretirementofUScurrent-listedairframes | — |
Mohajer-2 · Wingspan
Single source3.8 m (12 ft 6 in)[source]
Owndesignclaimedairframeweight, notgenericMicroUAV · Mass
Single source2 lb[source]Owndesignclaimedairframeweight, notgenericMicroUAV
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 · 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.
| Wing dimensions |
|---|
28 in[source]Literalwingsdimensionaxisnotnamed, notinventedwingspan |
| — |
| Launch and recovery | fully autonomous operation from launch to landing using waypoints[source] | — |
|---|
| Specification controversy | In 2015, Prioria vendor Condor Aerial alleged that Prioria was providing false specifications for the Maveric UAV[source]Retainexplicit source dispute, notapprovedcross-check | — |
|---|
| Country of origin | United States[source]Inventory Origin column; table 5, row 24, cell 3; revision 1377059256; retrieved 2026-09-30 | — |
|---|
| National origin | — | Iran[source] |
|---|
| Designer | — | Qods Aviation Industry Company[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Iran Syria Venezuela Hezbollah[source] |
|---|
| Number built | — | 253 (mid-2000s)[source] |
|---|
| Manufactured | — | 1980s–present[source] |
|---|
| Introduction date | — | February 1986[source] |
|---|
| First flight | — | 1985[source] |
|---|
| Capacity | — | 15 kg payload[source] |
|---|
| Propellers | — | 2-bladed[source] |
|---|
| Reported operators | — |
|
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