Role & capabilities
- Multiple mission configurations
- Primary domain
- Air
- System type
- Multirole aircraft
- Developer / manufacturer
- PR-DC
- Origin / production countries
- Serbia
- Other names
- No additional names recorded
- Variants / configurations
- IKA-20 official configuration; other mission-named IKA products not assumed identical
- Operators / programme customers
- Not identified in reviewed sources
Evidence & current status
Manufacturer identity is confirmed by the Serbian Ministry of Defence. Public sources do not establish a complete versioned IKA-20 specification set.
IKA-20 is a Serbian reusable multicopter attributed by the Ministry of Defence to PR-DC. The official description identifies a six-rotor composite aircraft with reconnaissance and defence roles. PR-DC’s family material confirms electric propulsion across the IKA product line.
The current manufacturer website organises offerings by mission names rather than supplying a complete IKA-20 technical table. Those marketed configurations are not automatically identical to the airframe described by the military. A model name containing a number is also not sufficient evidence of payload capacity or maximum take-off mass.
The catalogue therefore records the confirmed architecture and producer while leaving missing numerical fields explicit. It does not transfer specifications from IKA-MICRO, IKA-50 or another family member. Official presentation establishes the named programme, but a complete current fleet register, configuration acceptance and endurance under a specified load remain separate evidence requirements.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| Airframe | Six-rotor multicopter | Official IKA-20 description. Source |
| Launch / recovery | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Propulsion | Battery-electric IKA family | Family-level architecture; exact motor/battery configuration not established. Source |
| Dimensions | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Mass | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. 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 | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Altitude | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Payload | Not established in the reviewed public sources. | Public evidence gap. No estimate or neighbouring variant value has been substituted. Source |
| Sensors | Reconnaissance imaging | Installed sensor model undisclosed. 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.
- Serbian Ministry of Defence IKA-20 description (opens in a new tab)Government / operator
- PR-DC current IKA family overview (opens in a new tab)Manufacturer