Miniaturization model for UAVs Minimized Vibration & Noise by our technique Provide an electronic board Customized item for Military's needs

External SSD drive with total data delete option by hotkey or red button push Highly robust solution due to the use of a full-aluminium chassis Highly customizable Native supported four inputs for Full HD SDI cameras

Maintenance Increase security and productivity to reduce costs and minimize downtime. Willing to provide our customers with high-performance technical assistance, we offer scheduled and unplanned maintenance interventions, as well as periodic verification of measurement channels using our calibration equipments. Our systems allow us to perform these operations internally or at our customers site.

Supports non-destructive inspection of aircraft composite skin structures and is composed of a piezoelectric layer sensor, data acquisition equipment, and damage analysis software. Utilizes piezoelectric sensors to generate Lamb-wave and acquire signals, collecting data to accurately detect and assess composite damage. Visualizes inspection results on display such as damage location, size and index. - POD Accuracy: 1 inch 90% or more - POD Precision : Position error within 30 mm - 64 channels / 230 path reference detection time within 10 minutes - Sensor : Resonance resistance less than 400kΩ - Sensor : MIL-STD-810G - Sensor : RTCA DO-160 Section 23.0 - DAQ : x128 Piezoelectric sensor interface

The nose wheel assembly refers to the complete integrated unit consisting of the wheel, tire, axle, bearings, and associated structural components. In some configurations, it also includes steering mechanisms, shock absorbers (oleo strut), and braking systems (for specific aircraft types). The assembly is engineered for durability, precision, and reliability, enabling the aircraft to safely absorb impact forces during landing and provide accurate steering during taxiing.

Thermostatic Temperature switches

1. Maintenance • Depot Maintenance • Structure & Avionics Replacement, Repair, Wire Harness, Test and Inspection 2. Upgrade & Modification • Structure Upgrade and Modification • Avionics Upgrade, System Integration, Test and Inspection Highlights √ Final Assembly incl. Engine Installation √ System Integration, Test & Inspection Project Highlight : KT-100 & Light Sport Aircraft (Final Assembly), HH-60, CH-53, CH-47, F-16, P3-c, C-130H, AS-1S, MD500, NG RQ-4B ( Logistic & Ground Support)

- Operates by an internal pipeline open/close mechanism controlled by a solenoid valve - Relief plug: prevents malfunction due to internal pressure expansion - Manual discharge available via manual handle when power is OFF - Outputs an abnormal signal if the reference pressure drops due to extinguishing agent leakage