Role & capabilities
- Reconnaissance
- Primary domain
- Air
- System type
- Reconnaissance aircraft
- Developer / manufacturer
- Primoco UAV
- Origin / production countries
- Czech Republic
- Other names
- No additional names recorded
- Variants / configurations
- Not distinguished in reviewed sources
- Operators / programme customers
- Not identified in reviewed sources
Evidence & current status
Current corporate reporting supports production and deliveries; military certification and civil operator authorisation are distinct. Named military fleet totals remain undisclosed.
One 150 is Primoco’s Czech fixed-wing surveillance aircraft. The company’s 2026 investor material records aircraft deliveries and distinguishes aircraft sold from aircraft delivered. Those accounting measures should not be combined into a single fleet total, and company-wide deliveries do not provide a complete military operator inventory.
Primoco reports military certification to STANAG 4703 in March 2025. Its civil LUC authorisation concerns the operator framework and is a different approval. The catalogue records both accurately without treating a civil operating authorisation as a universal aircraft type certificate.
The current technical baseline separates flight distance from direct ground-station communications radius. Maximum payload is also a separate limit, not a guarantee for every fifteen-hour flight. The investor presentation discusses further electronic and other integrations as development activity. Those plans are not recast as already accepted capabilities of every delivered surveillance aircraft.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| Airframe | Fixed wing; short-runway operation | One 150 baseline. Source |
| Launch / recovery | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Propulsion | Piston engine | 2026 presentation. Source |
| Dimensions | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Mass | 150 kg maximum take-off | Supplier baseline. Source |
| Endurance | Up to 15 hours | Supplier baseline. Source |
| Range | Up to 1,800 km flight distance; 200 km direct-control radius | Distinct flight and communications measures. Source |
| Speed | 120 km/h cruise | 2026 presentation. Source |
| Altitude | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Payload | 1–30 kg | Payload and flight-duration limits are configuration dependent. Source |
| Sensors | Configurable optical, radar and other sensor equipment | Installed fit depends on customer configuration. Source |
| Communications / navigation | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
Publication history
- — Published reference update.
Suggest a correction to this entry
Follow the evidence
Source types identify who makes the claim. Programme milestones and supplier statements should be read in context.
- Primoco Q1 2026 investor presentation and aircraft baseline (opens in a new tab)Company regulatory / investor material
- Primoco manufacturer release: certification, 17 March 2025 (opens in a new tab)Manufacturer release archive