Role & capabilities
- Multiple mission configurations
- 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.
SINYAR LAR1 belongs to the Flaris–EDGE collaboration to adapt a piloted jet design for uncrewed missions. The companies announced the programme in November 2023. EDGE publishes a design baseline for SINYAR LAR1, while Flaris’s development history makes clear that the parent aircraft and the uncrewed programme have different milestones.
A flight or delivery of a piloted Flaris LAR1 does not by itself establish an autonomous SINYAR flight or military acceptance. Likewise, specifications associated with the later LAR3P presentation should not be silently substituted into this earlier configuration.
The profile records Poland and the UAE as programme origins, reflecting the named collaboration rather than counting a customer as a manufacturer. Published numerical values remain supplier design claims. Evidence of uncrewed flight, configuration certification, customer delivery and service entry should be recorded separately when available.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| 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 ↗ |
Publication history
- — Added in the September 2026 global coverage review, with sources, configuration limits and explicit data gaps.
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Follow the evidence
Source types identify who makes the claim. Programme milestones and supplier statements should be read in context.