Skylark I-LEX
Portable electric reconnaissance aircraft representing a later evolution of the Skylark I family.
- Country / region
- Israel
- Programme status
- Supplier-reported status
- Sources reviewed
- 21 Sept 2026
Supplier-reported statusSupplier-reported status
- Primary domain
- Air
- System type
- Reconnaissance aircraft
- Developer / manufacturer
- Elbit Systems
- Origin / production countries
- Israel
- Other names
- No additional names recorded
- Variants / configurations
- Skylark I-LEX; earlier Skylark I / I-LE data require dated configuration
- Operators / programme customers
- Not identified in reviewed sources
Evidence & current status
Supplier information is attributed; performance and operational acceptance require configuration-specific evidence.
Role & capabilities
- Reconnaissance
Specifications in context
- Airframe
- Portable fixed wing
I-LEX baseline.
Source ↗ - Launch / recovery
- Airbag-assisted recovery
Launch method not established by this source.
Source ↗ - Propulsion
- Electric
Current product page.
Source ↗ - Dimensions
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗ - Mass
- 7.5 kg take-off weight
Supplier baseline.
Source ↗ - Endurance
- Up to 3 hours
Maximum claim.
Source ↗ - Range
- 40 km line-of-sight communications
Not flight-path distance.
Source ↗ - Speed
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗ - Altitude
- 15,000 ft service ceiling
Supplier claim.
Source ↗ - Payload
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗ - Sensors
- Stabilised day/night imaging
Installed payload may vary.
Source ↗ - Communications / navigation
- Not established in the reviewed public sources.
Public evidence gap. No estimate or neighbouring variant value has been substituted.
Source ↗