
ADrones & UAVs
HESA Ababil
Ababil-1 : Loitering munition Ababil-2 Ababil-B : Target drone Ababil-S : Surveillance and reconnaissance Qasef-1 : Loitering munition Ababil-3 , Ababil-4 and Ababil-5 : Surveillance and reconnaissanc
Preparing your view.

ADrones & UAVs
Ababil-1 : Loitering munition Ababil-2 Ababil-B : Target drone Ababil-S : Surveillance and reconnaissance Qasef-1 : Loitering munition Ababil-3 , Ababil-4 and Ababil-5 : Surveillance and reconnaissanc
Measured figures
Ababil-2 · Length
Single source2.88 m (9 ft 5 in)[source]
Configuration
| Specification | HESA Ababil | SWAN III |
|---|---|---|
| Crew | none[source] | — |
| Type | Ababil-1 : Loitering munition Ababil-2 Ababil-B : Target drone Ababil-S : Surveillance and reconnaissance Qasef-1 : Loitering munition Ababil-3 , Ababil-4 and Ababil-5 : Surveillance and reconnaissance Armed variant: Combat drone[source] | Unmanned aerial vehicle[source] |
| National origin | Iran[source] | Estonia[source] |
| Manufacturer | HESA Isfahan factory Syrian Scientific Studies and Research Center (Ababil-3)[source] | — |
| Designer |
Ababil-2 · Wingspan
Single source3.25 m (10 ft 8 in)[source]
Ababil-2 · Height
Single source0.91 m (3 ft 0 in)[source]
Ababil-2 · Combat range
Single source120 km (75 mi, 65 nmi)[source]
Ababil-2 · 1 × WAE-342 twin-cylinder piston engine
Single source1 × WAE-342 twin-cylinder piston engine, 19 kW (25 hp)[source]
Ababil-2 · Wing area
Single source1.76 m 2 (18.9 sq ft)[source]
Ababil-2 · or higher
Single source3,000 m (9,800 ft) or higher[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Iran Aircraft Manufacturing Industrial Company[source]
ELI Military Simulations[source] |
| Status | In service[source] | Active[source] |
|---|
| Primary user | Iran Iraq Sudan Syria (Historical)[source] | Georgian Land Forces[source] |
|---|
| Number built | Unknown (Hundreds)[source] | Handful[source] |
|---|
| Manufactured | 1980s–present[source] | — |
|---|
| Introduction date | disputed[source] | 2012[source] |
|---|
| First flight | 1986[source] | 2011[source] |
|---|
| Capacity | 40 kg payload[source] | — |
|---|
| Fuel capacity | 16 liters[source] | — |
|---|
| Endurance | 1 ¼ – 2 hr[source] | — |
|---|
| Propellers | 2-bladed[source] | — |
|---|
| Developed from | — | 2012[source] |
|---|
| Reported operators |
| — |
|---|