Technical Direction
Public specifications are intentionally high level. Detailed engineering, drawings and validation materials are available only under appropriate confidentiality arrangements.
4-cornerindependently controlled air-ride suspension with closed-loop feedback
130 PSIonboard compressor system with regulated pneumatic circuits
21700lithium-ion cell architecture with integrated battery management
20 + 20 kmtarget range with an optional auxiliary range module
930 mmcompact platform length target for manoeuvrability
Thermalactive battery and compartment heating-and-cooling architecture
ROS 2robotics software direction for autonomy and sensor integration
UGVmission-package adaptability for rugged unmanned ground applications
Integrated Controls
Closed-loop sensing and supervisory control are intended to coordinate suspension response, platform stability, ride height, power systems and mission-specific functions.
Configuration-Based Validation
Machine-level performance will be established through prototype assembly, calibration, payload testing, thermal evaluation and field validation for each operating configuration.
Technical Materials
Detailed materials are controlled.
Qualified investors, lenders, strategic partners and institutional groups may request additional technical and commercial information.