Role & capabilities
- Remote demining
- Interchangeable engineering attachments
- Primary domain
- Land
- System type
- Explosive-ordnance disposal robot
- Developer / manufacturer
- SKB MO RF
- Origin / production countries
- Russia
- Other names
- MRTK-R Uran-6; Уран-6
- Variants / configurations
- Not distinguished in reviewed sources
- Operators / programme customers
- Russian armed forces
Evidence & current status
Current manufacturer lists use and specifications. Catalogue does not reproduce unsupported absolute safety claims. Current fleet size and dated configuration changes remain unverified.
Uran-6 is a tracked engineering robot intended to separate personnel from hazardous demining work. The current manufacturer, SKB MO RF, describes a radio-controlled vehicle with interchangeable working equipment, rather than a general-purpose autonomous combat robot. Its tasks and design should therefore be kept separate from the armed Uran-9 despite the shared family name.
The manufacturer documents acceptance trials and participation in demining work in Syria. A Russian Ministry of Defence video also records deployment of Uran-6 in 2020. These sources establish actual use, but neither supplies a reliable current fleet total or a complete record of subsequent upgrades.
The published dimensions and mass describe the manufacturer's offered vehicle. Attachments and transport equipment can change the dimensions of a complete deployed system. Camera-assisted remote operation is documented; this is not evidence that the robot independently decides where or how to clear explosive hazards. The manufacturer's present identity is recorded without assuming that every historical corporate attribution refers to an unchanged legal entity.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| Configuration | Tracked remote demining platform | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Mobility | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source ↗ |
| Dimensions | 4,565 × 2,015 × 1,470 mm | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Mass | 6 tonnes equipped mass | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Payload | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source ↗ |
| Endurance | 5 hours per refuelling | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Range | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source ↗ |
| Speed | Up to 5 km/h | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Terrain / environment | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source ↗ |
| Sensors | Four cameras for surrounding views | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Communications / control | Radio remote control | Supplier-published configuration; independent acceptance test not established. Source ↗ |
| Launch / deployment | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. 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.