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.

GIDS Scout V30

A small electric fixed-wing VTOL reconnaissance aircraft offered separately from GIDS' Scout quadcopters.

Country / region
Pakistan
Programme status
Supplier-reported status
Sources reviewed
21 Sept 2026
Supplier-reported statusSupplier-reported status
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Global Industrial & Defence Solutions
Origin / production countries
Pakistan
Other names
No additional names recorded
Variants / configurations
Not distinguished in reviewed sources
Operators / programme customers
Not identified in reviewed sources

Evidence & current status

No named service operator established. Cruise altitude is not used as a ceiling.

Role & capabilities

  • VTOL reconnaissance
  • Day/night observation
  • Wing-borne cruise

Specifications in context

Airframe
Not established in the reviewed public sources.

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

Source
Launch / recovery
Not established in the reviewed public sources.

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

Source
Propulsion
Electric

Supplier specification; no independent performance validation established.

Source
Dimensions
3 m wingspan; 1.8 m length

Supplier specification; no independent performance validation established.

Source
Mass
17 kg maximum take-off weight

Supplier specification; no independent performance validation established.

Source
Endurance
Up to 3.5 hours

Supplier specification; no independent performance validation established.

Source
Range
Not established in the reviewed public sources.

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

Source
Speed
65–80 km/h cruise

Supplier specification; no independent performance validation established.

Source
Altitude
Not established in the reviewed public sources.

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

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
50 km control radius

Manufacturer control-radius term; not flight distance.

Source