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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
At a glance
Measured figures
Ababil-2 · Length
Single source2.88 m (9 ft 5 in)[source]
Length
Single sourceConfiguration
| Specification | HESA Ababil | Pegaz |
|---|---|---|
| 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 combat aerial vehicle[source] |
| National origin | Iran[source] | Serbia[source] |
| Manufacturer | HESA Isfahan factory Syrian Scientific Studies and Research Center (Ababil-3)[source] | Utva Aviation Industry[source] |
5.395 m (17 ft 8 in)[source]
Cruise; Ababil-2 · Cruise speed
Single sourceMaximum; Ababil-2 · in level flight
Single source370 km/h (230 mph, 200 kn) in level flight[source]
250–305 km/h (155–190 mph, 135–165 kn)[source]
Cruise; Cruise speed
Single sourceMaximum; Maximum speed
Single sourceexact maximum range is yet unknown
Single source250 km (160 mi, 130 nmi) exact maximum range is yet unknown[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Iran Aircraft Manufacturing Industrial Company[source] | Military Technical Institute[source] |
|---|
| Status | In service[source] | In service[source] |
|---|
| Primary user | Iran Iraq Sudan Syria (Historical)[source] | Serbian Air Force and Air Defence[source] |
|---|
| Number built | Unknown (Hundreds)[source] | 12+[source] |
|---|
| Manufactured | 1980s–present[source] | 2011–present[source] |
|---|
| Introduction date | disputed[source] | 2025[source] |
|---|
| First flight | 1986[source] | 2011[source] |
|---|
| Capacity | 40 kg payload[source] | 50 kg (110 lb) payload[source] |
|---|
| Fuel capacity | 16 liters[source] | — |
|---|
| Propellers | 2-bladed[source] | 2-bladed pusher propeller[source] |
|---|
| Rockets | — | 2 × FT-8D laser guided rocket[source] |
|---|
| Reported operators |
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|
|---|
245 kg (540 lb)[source]