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 ↗