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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.

Hermes 650 Spark

Tactical surveillance aircraft with documented customer testing and a separately proposed maritime operating concept.

Country / region
Israel
Programme status
Development / trials
Sources reviewed
21 Sept 2026
Development / trialsDevelopment / trials
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Elbit Systems
Origin / production countries
Israel
Other names
No additional names recorded
Variants / configurations
Land-based aircraft programme; Maritime Apparatus — July 2026 integration concept
Operators / programme customers
Not identified in reviewed sources

Evidence & current status

Supplier reports customer testing; July 2026 ship concept does not establish operational maritime acceptance.

Role & capabilities

  • Reconnaissance

Specifications in context

Airframe
Fixed wing with front-mounted engine

Spark architecture.

Source
Launch / recovery
Short-runway take-off and landing

Aircraft feature; maritime deployment remains a concept.

Source
Propulsion
Not established in the reviewed public sources.

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

Source
Dimensions
Not established in the reviewed public sources.

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

Source
Mass
Not established in the reviewed public sources.

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

Source
Endurance
Up to 24 hours

Supplier maximum.

Source
Range
300 km line-of-sight datalink; SATCOM option

Communications limits, not ferry range.

Source
Speed
Not established in the reviewed public sources.

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

Source
Altitude
Not established in the reviewed public sources.

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

Source
Payload
260 kg useful-load allowance

Useful load is not assumed to be sensor payload excluding fuel.

Source
Sensors
EO/IR/SWIR, radar and electronic-intelligence options

Configuration-dependent.

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

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

Source