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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.

KUS-FT

A South Korean tactical fixed-wing reconnaissance UAV with documented military operation, automatic flight and short-distance recovery.

Country / region
South Korea
Programme status
In service / use documented
Sources reviewed
20 Sept 2026
In service / use documentedIn service / use documented
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Korean Air
Origin / production countries
South Korea
Other names
KUS FT; Korean Air tactical UAV
Variants / configurations
KUS-FT fixed-wing system; VTOL successor concepts are separate
Operators / programme customers
Republic of Korea Army; Republic of Korea Marine Corps

Evidence & current status

Manufacturer identifies military operators. Zero-filled brochure fields are treated as undisclosed, not valid numerical data.

Role & capabilities

  • Reconnaissance aircraft

Specifications in context

Airframe
Fixed-wing tactical UAV

Supplier-published figure; configuration and operating conditions affect performance.

Source ↗
Launch / recovery
Automated take-off and short-distance landing; emergency parachute

Supplier-published figure; configuration and operating conditions affect performance.

Source ↗
Propulsion
35 hp rotary engine

Supplier-published figure; configuration and operating conditions affect performance.

Source ↗
Dimensions
3.7 m long; 4.5 m span; 0.9 m high

Supplier-published figure; configuration and operating conditions affect performance.

Source ↗
Mass
150 kg maximum take-off weight

Supplier-published figure; configuration and operating conditions affect performance.

Source ↗
Endurance
Not established from the reviewed public sources.

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

Source ↗
Range
Not established from the reviewed public sources.

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

Source ↗
Speed
200 km/h maximum; 130 km/h cruise

Supplier-published figure; configuration and operating conditions affect performance.

Source ↗
Altitude
Not established from the reviewed public sources.

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

Source ↗
Payload
Not established from the reviewed public sources.

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

Source ↗
Sensors
EO/IR

Supplier-published figure; configuration and operating conditions affect performance.

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

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

Source ↗