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 ↗