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The mRO-50 Ruggedized is a breakthrough microwave optical double resonance (MODR) low SWaP-C Miniaturized Rubidium Oscillator designed to meet the latest commercial, military and aerospace requirements where time stability and power consumption are critical. It provides a one day holdover below 1µs and a retrace below 1E-10 in a form factor (50.8 x 50.8 x 20mm) that takes up only 51 cc of volume (about one-third of the volume compared to standard rubidiums) and consumes only 0.36W of power, which is about ten times less than existing solutions with similar capabilities. The mRO-50 Ruggedized Oscillator provides accurate frequency and precise time synchronization to mobile applications, such as military radio-pack systems in GNSS-degraded or denied environments. Its wide-ranging operating temperature of -40° to +80°C is also ideal for: Underwater Applications, Military Communications, Radars, Low Earth Orbit, Electronic Warfare, Airbornes & Avionics, UAV/UGV/USV/UUV

This miniature fin actuator manufactured by MPS Microsystems was designed based on customer specifications. Designed to guide a very small object and disposing of an extremely limited space, it meets 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.

Harness Quantum Power for Exceptional Performance! IQM's most advanced superconducting quantum computing platform. It is immediately available with 20 high-fidelity qubits, easily upgradable to 54, and soon up to 150 qubits.

To reduce aircraft development lead-time, Safran Engineering Services is specialized in quick design and engineering in full autonomy. Teams provide global loads for ground and flight maneuvers, follows the evolution of weight and center of gravity for aircraft components and support sales campaigns with weight & balance evaluation.

Hyundai Elevator is leveraging its expertise in elevator technology to develop infrastructure for urban air mobility (UAM). We are working on takeoff, landing, charging, and maintenance platforms that can be built on top of existing buildings, solving space constraints in congested urban environments. Our initiative is backed by their manufacturing expertise and government support, though global building codes may present a challenge in scaling the solution.

The AMT-206-1 composite tail rotor blade is a direct replacement for Bell 206A and 206B series helicopter tail rotor blades. Now fitted with a new style of feathering bearings manufactured by KAMATICS. These bearings provide a longer life expectancy, with a patented lining that provides lighter pedal loads and a higher level of chemical resistance, compared to that of the standard fabric Teflon-lined bearings. The AMT-206-1 tail rotor blade has a non-symmetrical airfoil section and incorporates a swept tip. The T/R Blade is primarily fabricated from uni-directional Graphite (carbon fiber) and Aramid (Kevlar™) continuous fibers suspended in an epoxy matrix and is fitted with a nickel abrasion strip on the leading edge. The abrasion strip is bonded on using a urethane adhesive. The AMT-206-1 composite tail rotor blades have a 30% cost advantage, twice the lifespan, higher strength and thrust, and a substantial noise reduction, making them safer and ideal for helicopter operators flying in noise-sensitive areas like national parks and built-up areas.

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.