VECTORDEFENCE DRONE
INTELLIGENCE
INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
Editor

DEFENCE DRONES / THE LIBRARY

Compare the evidence.

Choose up to three systems. Specifications retain their source and configuration; missing information is left undisclosed.

Bayraktar TB2

An established medium-altitude aircraft combining reconnaissance sensors and an armed mission option. The TB2 family is distinct from Baykar's larger Akıncı and newer jet programmes.

Country / region
Türkiye
Programme status
Use documented
Sources reviewed
20 Sept 2026
In service / use documentedUse documented
Primary domain
Air
System type
Multirole aircraft
Developer / manufacturer
Baykar
Origin / production countries
Türkiye
Other names
No additional names recorded
Variants / configurations
TB2-A; TB2-B; TB2-C; TB2-D
Operators / programme customers
No complete operator list disclosed in the reviewed sources

Evidence & current status

The cited public record documents military use or operator acceptance. Specifications still depend on the particular production version and mission configuration.

Role & capabilities

  • Persistent EO/IR observation
  • Automatic flight functions
  • Armed configurations

Specifications in context

Airframe
Fixed-wing multirole aircraft

Published supplier specification; configuration and conditions affect performance.

Source ↗
Launch / recovery
Automatic runway take-off, landing and taxi

Published supplier specification; configuration and conditions affect performance.

Source ↗
Propulsion
100 hp internal-combustion engine

Published supplier specification; configuration and conditions affect performance.

Source ↗
Dimensions
12 m span; 6.4 m length; 2.2 m height

Published supplier specification; configuration and conditions affect performance.

Source ↗
Mass
700 kg MTOW in current table

Published supplier specification; configuration and conditions affect performance.

Source ↗
Endurance
18+ h current specification; 27 h 3 min is a separate flight record

Published supplier specification; configuration and conditions affect performance.

Source ↗
Range
Not established from the reviewed sources.

Public data gap; no estimate substituted. Follow the source for subsequent releases.

Source ↗
Speed
90 KTAS cruise; 110 KTAS maximum

Published supplier specification; configuration and conditions affect performance.

Source ↗
Altitude
16,000 ft operational; 20,000 ft ceiling

Published supplier specification; configuration and conditions affect performance.

Source ↗
Payload
150 kg

Published supplier specification; configuration and conditions affect performance.

Source ↗
Sensors
EO/IR or surveillance-radar options

Published supplier specification; configuration and conditions affect performance.

Source ↗
Communications / navigation
LOS/BLOS options; sensor-fusion navigation

Published supplier specification; configuration and conditions affect performance.

Source ↗