
S4 Platform
Dual-Use, UAV Drone
Built to perform,
any way you need it to.
Developed by aerospace research engineers backed by The Levyne Group (R&D), the S4 is an experimental fast flight platform designed to be compatible with two propulsion systems, jet turbine or propeller. Sharing a common fuselage and aerodynamic form, it provides a versatile testbed for advancing packaging, wingspan dynamics, and propulsion integration in next-generation UAV design.
Key Data
220Nm
Maximum Thrust produced @100% power (Jet)
5.2KG
Total carbon fibre airframe weight
1.40m
Maximum length
420mph
Theoretical top speed

Design & Engineering

Composite Construction
Aerospace-grade carbon fiber and advanced composites were used throughout the S4, providing unmatched strength-to-weight performance. They maintained rigidity under high-speed loads, optimized efficiency for both propulsion systems, and enabled precise shaping of the body for peak aerodynamic performance.
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CAD/CAM
This helped model every detail of the airframe, including the sophisticated airfoil shapes of the blended body, with exacting tolerances. This strategy ensures that complex curves, aerodynamic surfaces, and structural elements were manufactured with accuracy, allowing the S4 to achieve optimal performance while maintaining design integrity.

PROPULSION
Designing the S4 to accommodate two different propulsion systems introduced several challenges, from differences in vibration and weight distribution to airflow variations. While one configuration prioritises maximum speed, the other was optimises for endurance.
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PACKAGING/ASSEMBLY
Packaging and assembly of the S4 demanded meticulous attention to tight-fitting components and manufacturability. Each part was designed to balance weight, flex under load, and aerodynamic constraints on external surfaces.













