Role & capabilities
- Collaborative aircraft
- Autonomous runway taxi, take-off and landing
- Advertised EO, infrared search-and-track and AESA radar options
- Primary domain
- Air
- System type
- Collaborative aircraft
- Developer / manufacturer
- Baykar
- Origin / production countries
- Türkiye
- Other names
- No additional names recorded
- Variants / configurations
- Prototype/test aircraft; S2 production-model test aircraft; Further advertised configurations are not all demonstrated
- Operators / programme customers
- No complete operator list disclosed in the reviewed sources
Evidence & current status
Public demonstrations or flight tests establish development activity, not full operational service. Advertised performance is not a complete independent test result.
Role & programme
A jet-powered uncrewed combat-aircraft programme. July 2026 reporting documents testing of an S2 production-model aircraft, while development and integration work continue.
A production-model test aircraft is not evidence of operational military acceptance. Baykar’s current product page advertises high-subsonic performance and a 500-nautical-mile combat radius. That radius is a different measure from ferry range or datalink reach. Advertised future configurations and mission sensors remain separate from the particular aircraft involved in each flight test.
Sourced specifications
Figures apply to the named configuration. Maximum values are not guaranteed operating performance.
| Specification | Reported value | Context & source |
|---|---|---|
| Airframe | Jet-powered uncrewed combat aircraft | Published supplier specification; configuration and conditions affect performance. Source |
| Launch / recovery | Autonomous runway taxi, take-off and landing | Published supplier specification; configuration and conditions affect performance. Source |
| Propulsion | Turbofan | Published supplier specification; configuration and conditions affect performance. Source |
| Dimensions | 10 m span; 14.5 m length; 3.5 m height | Published supplier specification; configuration and conditions affect performance. Source |
| Mass | 8,500 kg maximum take-off mass | Published supplier specification; configuration and conditions affect performance. Source |
| Endurance | 3+ h | Published supplier specification; configuration and conditions affect performance. Source |
| Range | 500 nmi combat radius | Published supplier specification; configuration and conditions affect performance. Source |
| Speed | Mach 0.6 cruise; Mach 0.9 maximum | Published supplier specification; configuration and conditions affect performance. Source |
| Altitude | 25,000 ft operational; 40,000 ft ceiling | Published supplier specification; configuration and conditions affect performance. Source |
| Payload | 1,500 kg | Published supplier specification; configuration and conditions affect performance. Source |
| Sensors | Advertised EO, infrared search-and-track and AESA radar options | Published supplier specification; configuration and conditions affect performance. Source |
| Communications / navigation | LOS and BLOS communications | Published supplier specification; configuration and conditions affect performance. Source |
Documented milestones
S2 test update published
Manufacturer described July 2026 integration tests; not operational acceptance.
Read the announcement
Publication history
- — Expanded catalogue profile with sourced specifications, variant distinctions, programme evidence and explicit public 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.
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