Low Size, Weight and Power (SWaP) at only 297g. Up to 100 TOPS GPU by NVIDIA® Jetson Orin™ NX Supports multiple camera and sensor interfaces 2x GbE and 2x USB3 for RGB/ Infrared/ hyperspectral cameras and lidar/ radar 2x GMSL2 for HDR/ 3D cameras Built-in UART and CAN to interact with flight controller 1x M.2 2230 for storage and 4G/5G communication ready Supports 4S-14S drone battery pack Compatible GMSL2 cameras with pre-built drivers

Titanium Grade 1 Strip Titanium Grade 2 Bars-Sheets and Plates-Tubes and Pipes Titanium Grade 5 ELI Bars-Sheets and Plates Titanium Ti-6Al-7Nb Bars

Weight Reduction: Eliminates complex hydraulic lines, pumps, and fluids, thereby reducing overall aircraft weight. Maintenance Efficiency: Simplifies maintenance requirements by removing hydraulic components that are prone to leakage and degradation. Improved Reliability: Provides precise braking control with fewer mechanical parts, resulting in higher system reliability and reduced downtime. Integration with Advanced Systems: Enables seamless connection with modern avionics and aircraft health monitoring systems, supporting predictive maintenance and optimized performance.

FINISHED THE DEVELOPING / INTEGRATED THE 2CH. FORJ Specification MODEL: SREM-1466-012 APPLICATION: SONAR WINCH SIZE: Φ140(O.D) / 664(H) NO. OF RINGS: 128RINGS TYPE: END ROTATING: CW/CCW

This Control Actuation System (CAS) is a guidance system for unmanned flying objects. It consists of three MPS fin actuators that each independently position an aerodynamic fin. The maximum angle of incidence is ±8°, which allows the device to carry out highly precise dynamic manoeuvres. The miniature fin actuators that make up this Control Actuation System are manufactured by MPS Microsystems and were designed based on customer specifications. Designed to guide a very small object and disposing of an extremely limited space, these fin actuators meet strict requirements in terms of performance, weight - less than 100 g - and dimensions. To reduce the length of this actuator, MPS Microsystems used part of the screw length as the motor axis. This screw is equipped with a very compact 4-point contact bearing that simultaneously absorbs axial and radial loads. The angular play on the aileron axis is less than 0.1° rms. This actuator meets the storage and vibration requirements of military equipment.

Temperature Calibrated Pressure Sensors The Air Data Unit features very high accuracy absolute and differential pressure sensors. These are factory calibrated over a wide temperature range to further increase measurement accuracy and provide the best air data possible through varying conditions. Power Up Self-Calibration On top of factory temperature calibration, every time the air data unit powers up, it performs a self excitation calibration to adjust for small deviations of bias and scaling error. This allows the system to compensate for calibration aging and means that it never needs to be returned to the factory for recalibration. Reliability The Air Data Unit is built on top of a safety oriented real time operating system and all software is designed and tested to safety standards with fault tolerance. Its communication interface is optically isolated and the hardware is designed and tested to MIL spec.

Engine Parts, Overhaul

It can carry and deliver payloads of 5 to 10 kilograms, making it suitable for commercial and industrial logistics. The drone has been successfully tested in extreme environments, ensuring stable performance under harsh conditions. With its proven capability, PELICAN expands the possibilities of drone-based delivery solutions in both urban and remote areas.