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BDrones & 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 | ENICS Eleron-10 | HESA Ababil |
|---|---|---|
| Crew | — | none[source] |
| Role | medium-range reconnaissance UAV for 24/7 surveillance,[source] | — |
| Source manufacturer statement | The first prototype of the drone was developed and manufactured by ENICS on 8 January 2011 as a successor to the smaller Eleron-3 .[source]Only the subject, component or variant named in this passage; unresolved names do not create a manufacturer identity | — |
| 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] |
| National origin | — | Iran |
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.
| Manufacturer | — | HESA Isfahan factory Syrian Scientific Studies and Research Center (Ababil-3)[source] |
|---|
| Designer | — | Iran Aircraft Manufacturing Industrial Company[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary user | — | Iran Iraq Sudan Syria (Historical)[source] |
|---|
| Number built | — | Unknown (Hundreds)[source] |
|---|
| Manufactured | — | 1980s–present[source] |
|---|
| Introduction date | — | disputed[source] |
|---|
| First flight | — | 1986[source] |
|---|
| Capacity | — | 40 kg payload[source] |
|---|
| Fuel capacity | — | 16 liters[source] |
|---|
| Endurance | — | 1 ¼ – 2 hr[source] |
|---|
| Propellers | — | 2-bladed[source] |
|---|
| Reported operators | — |
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