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.

Korean Air KUS-VT

Korean Air's tiltrotor surveillance development, separately documented from the lift-and-cruise KUS-VS.

Country / region
South Korea
Programme status
Development / trials
Sources reviewed
21 Sept 2026
Development / trialsDevelopment / trials
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Korean Air Aerospace
Origin / production countries
South Korea
Other names
No additional names recorded
Variants / configurations
Not distinguished in reviewed sources
Operators / programme customers
Not identified in reviewed sources

Evidence & current status

Brochure placeholders for mass, payload, engine power, range and endurance are omitted. Continuous system coverage is not individual-aircraft endurance.

Role & capabilities

  • Tiltrotor flight
  • VTOL surveillance
  • Maritime observation offering

Specifications in context

Airframe
Tiltrotor

Supplier specification; no independent performance validation established.

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
3.5 m length; 5.2 m published width

Supplier specification; no independent performance validation established.

Source
Mass
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Endurance
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Range
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Speed
220 km/h maximum; 200 km/h cruise

Supplier specification; no independent performance validation established.

Source
Altitude
4.5 km published ceiling

Supplier specification; no independent performance validation established.

Source
Payload
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Sensors
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source
Communications / navigation
Not established in the reviewed public sources.

Public evidence gap. No estimate or neighbouring variant value has been substituted.

Source