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.

DRDO Archer

Indian piston-powered tactical aircraft documented in DRDO's export catalogue; distinct from the larger Archer-NG programme.

Country / region
India
Programme status
Supplier-reported status
Sources reviewed
21 Sept 2026
Supplier-reported statusSupplier-reported status
Primary domain
Air
System type
Multirole aircraft
Developer / manufacturer
DRDO / Aeronautical Development Establishment
Origin / production countries
India
Other names
No additional names recorded
Variants / configurations
Not distinguished in reviewed sources
Operators / programme customers
Not identified in reviewed sources

Evidence & current status

Catalogue evidence only. Archer-NG specifications and forecast first-flight dates are not transferred to Archer.

Role & capabilities

  • Tactical observation
  • Automatic runway operations
  • Configurable mission equipment

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
Piston engine using aviation gasoline

Supplier baseline; performance depends on payload and conditions.

Source
Dimensions
Not established in the reviewed public sources.

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

Source
Mass
Approximately 750 kg in the listed electro-optical configuration

Catalogue configuration weight; not identified here as a universal maximum take-off mass.

Source
Endurance
10–12 hours

Supplier baseline; performance depends on payload and conditions.

Source
Range
250 km (catalogue term)

The source does not establish a mission radius or data-link definition.

Source
Speed
Maximum 135 knots / approximately 250 km/h

Supplier baseline; performance depends on payload and conditions.

Source
Altitude
22,000 ft

Supplier baseline; performance depends on payload and conditions.

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