ALPAGU-B
Larger ALPAGU derivative unveiled in May 2026 with its own mass, duration and communications baseline.
- Country / region
- Türkiye
- Programme status
- Concept / announced
- Sources reviewed
- 21 Sept 2026
- Primary domain
- Air
- System type
- Loitering munition
- Developer / manufacturer
- STM
- Origin / production countries
- Türkiye
- Other names
- No additional names recorded
- Variants / configurations
- Not distinguished in reviewed sources
- Operators / programme customers
- Not identified in reviewed sources
Evidence & current status
Supplier information is attributed; performance and operational acceptance require configuration-specific evidence.
Role & capabilities
- Loitering munition programme
Specifications in context
- Airframe
- Fixed wing
ALPAGU-B, not original ALPAGU.
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
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗ - Mass
- 20 kg platform weight
Loading basis as supplied.
Source ↗ - Endurance
- 30 minutes
Supplier baseline.
Source ↗ - Range
- 40 km line-of-sight communications
Not total flight distance.
Source ↗ - Speed
- 25 m/s cruise
Supplier baseline.
Source ↗ - Altitude
- 500 m AGL mission height
Not a service ceiling.
Source ↗ - Payload
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗ - Sensors
- EO/IR imaging
Current product table.
Source ↗ - Communications / navigation
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗