VECTORDEFENCE DRONE
INTELLIGENCE
INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
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DEFENCE DRONES / THE LIBRARY

Compare the evidence.

Choose up to three systems. Specifications retain their source and configuration; missing information is left undisclosed.

JENIAH

Emirati uncrewed combat-aircraft programme with a published design baseline; exhibition and product material do not establish operational acceptance.

Country / region
United Arab Emirates
Programme status
Concept / announced
Sources reviewed
21 Sept 2026
Concept / announcedConcept / announced
Primary domain
Air
System type
Concept aircraft
Developer / manufacturer
ADASI / EDGE
Origin / production countries
United Arab Emirates
Other names
No additional names recorded
Variants / configurations
JENIAH development programme
Operators / programme customers
Not identified in reviewed sources

Evidence & current status

Unveiling and design specifications are established. Full-scale flight validation, delivered numbers and operational acceptance are not established by these sources.

Role & capabilities

  • Aircraft technology development

Specifications in context

Airframe
Jet-powered uncrewed combat-aircraft design

Supplier programme description.

Source
Launch / recovery
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Propulsion
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Dimensions
7 m wingspan; 11 m length

February 2025 design sheet.

Source
Mass
Above 4,000 kg maximum take-off mass

Advertised design figure.

Source
Endurance
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Range
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Speed
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Altitude
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Payload
480 kg

Supplier design capacity, not independently validated.

Source
Sensors
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Communications / navigation
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source