An Angle of Attack (AOA) indicator is a flight instrument that shows a pilot the angle between the aircraft's wing and the oncoming air, providing a crucial safety margin by warning of an approaching aerodynamic stall. Unlike airspeed. A Vertical Speed Indicator (VSI), also known as a Rate of Climb and Descent Indicator (RCDI) is an instrument which indicates the rate of climb or descent of an aircraft. These devices are installed and compatible with F-16 series aircraft and KAI's T-50/FA-50 series aircraft.

Hydraulic top bracing is an attenuation device installed between the main engine and the hull of the ship to reduce thermal expansion and vibration from the main engine to natural frequencies. The operating principle is an automatic control operating system through in/out and on/off the operating range of the hydraulic top bracing according to the rpm of the main engine. The number of hydraulic cylinders per engine is typically 2, 4, 6 depending on the type of engine, up to 8 are installed if necessary, and 1~2 of control panels are installed.

1. KAEMS is capable of providing C~D level Heavy Checks & Painting with Repairing/Modification. 2. With optimized process KAEMS always ensures the outbound date with customers upon trust. 3. Current capability NB : B737/A320 Upcoming capability WB : B787/B777/A350 [Hangar] - Base Maintenance Hangar : 4 Bay(B737 & A320) - Back Shop : Sheet Metal & Composite & Avionic Shop + ETC Component shop - Wash Bay : 1 Bay - Paint shop : component & entire painting(B737/A320/A321) [Customer] - Korea Low Cost Carrier - Cebu Pacific - Peach Aviation

ㅇKey Features RF Front-End - Frequency : C-Band - Tx Power : +27 dBm(0.5 W) , Rx Range : -10 ∼ -100 dBm - Rx Sensitivity : -95 dBm@2 MHz Baseband & Modem - Downlink : 2.4 Mbps / Uplink: 8 kbps - QPSK waveform and CTC Forward Error Correction Anti-Jamming / Anti-Spoofing / Video CODEC - Anti-Jamming Capability using DSSS - Anti-Spoofing Capability by AES-256/ ARIA-256 Encryption - Support H.264 / up to 1920x1080x30f Interface - 10/100 Base-T Ethernet x1, RS-422 x1, RS-232 x2 - 3G-SDI Digital Video IN/OUT Interface - Limited Discrete I/O (1PPS/sync_in, reset_in, status_out) ㅇQuality and Certification - MIL-STD-810G - MIL-STD-461F

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.

The TAC-450 FOG offers exceptional performance in bias stability, scale factor, and angle random walk, and is available in nine configurations to solve the most challenging design projects. The TAC-450 FOG is ideal for air, land, or maritime stabilization and pointing applications. Due to its versatility, and accurate, reliable output, it can also be utilized in navigation, guidance, and control systems. Highlights Designed for maximum ease of integration with housed or unhoused (for OEM configurations) options Available in nine configurations to solve the most challenging design projects Exceptional performance in bias stability, scale factor, and angle random walk 1-, 2-, or 3-axis configuration, each employing the world’s smallest precision FOG Technology Details Photonic Integrated Chip Technology EMCORE’s photonic integrated chip (PIC) technology* reimagines FOG technology by replacing individual fiber components with an innovative integrated planar optic chip. This results in a FOG with PIC Inside™ that’s reliable and robust. With three of these integrated photonic gyros at its core, the TAC-450-360 IMU provides the safe, accurate performance autonomous platforms demand.

We are recognized domestically and internationally for our technology and quality by supplying turbocharger parts and other parts that require high reliability and technology to ship and engine manufacturers .

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.