VECTORDEFENCE DRONE
INTELLIGENCE
INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
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DEFENCE DRONES / THE LIBRARY

Compare the evidence.

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

FT-5 / GLADIUS reconnaissance component

Polish tactical reconnaissance aircraft that forms the reusable sensor component of the wider GLADIUS system.

Country / region
Poland
Programme status
Order / production commitment
Sources reviewed
20 Sept 2026
Order / production commitmentOrder / production commitment
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Flytronic / WB GROUP
Origin / production countries
Poland
Other names
No additional names recorded
Variants / configurations
FT-5 IMINT; FT-5 ELINT; FT-5 SAR
Operators / programme customers
Poland — GLADIUS customer

Evidence & current status

Published performance is supplier-reported and configuration dependent; operational use does not independently validate every specification.

Role & capabilities

  • Reconnaissance aircraft

Specifications in context

Airframe
Fixed-wing tactical reconnaissance aircraft

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Launch / recovery
Runway take-off and automatic landing

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Propulsion
Two independently controlled fuel-injected engines

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Dimensions
6.4 m span; 3.1 m length

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Mass
85 kg brochure weight; precise mass definition not stated

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Endurance
Up to 10 hours

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Range
150 km radio line-of-sight

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Speed
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗
Altitude
5,000 m AMSL

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Payload
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗
Sensors
EO/IR; SAR and electronic-intelligence variants

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Communications / navigation
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗