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.

SINYAR LAR1

Polish–Emirati programme to develop an uncrewed aircraft from the Flaris jet lineage.

Country / region
Poland / United Arab Emirates
Programme status
Concept / announced
Sources reviewed
21 Sept 2026
Concept / announcedConcept / announced
Primary domain
Air
System type
Multirole aircraft
Developer / manufacturer
Flaris / EDGE
Origin / production countries
Poland / United Arab Emirates
Other names
No additional names recorded
Variants / configurations
SINYAR LAR1
Operators / programme customers
Not identified in reviewed sources

Evidence & current status

Uncrewed development programme; parent-aircraft piloted flights and deliveries do not establish SINYAR operational acceptance.

Role & capabilities

  • Multiple mission configurations

Specifications in context

Airframe
Not established in the reviewed public sources.

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

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
8.7 m span; 8.3 m length

SINYAR LAR1 product table.

Source
Mass
2,200 kg maximum take-off mass

Supplier design baseline.

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
545 km/h cruise

Supplier figure.

Source
Altitude
30,000 ft cruise altitude

Not a verified operational ceiling.

Source
Payload
450 kg

Advertised capacity.

Source
Sensors
Not established in the reviewed public sources.

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

Source
Communications / navigation
Satellite communications advertised

Programme offering; delivered equipment not confirmed.

Source