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 ↗