< Frequency Range > ● 500 ~ 2700 MHz < Output Power (W) > ● 100 < Gain (db) > ● 50 < Power Supply (V) > ● 32.5 < Current (A) > ● 14 < Dimension > ● 208.3 x 91.4 x 26.9 (mm)

Sungjin Techwin develops operating control computers designed for ground and naval defense applications. Engineered for harsh environments, these ruggedized systems provide secure and real-time processing to support RCWS operations, anti-drone defense, and unmanned surface vehicle control. Built to military standards, they offer high reliability under shock, vibration, and temperature extremes while enabling seamless integration with sensors, weapons, and communication networks. By combining durability with scalable architecture, Sungjin’s operating control computers ensure mission effectiveness across diverse modern battlefield domains.

The intelligent operations you didn't know existed - and didn't know you needed. Let data be your co-pilot with Honeywell Forge industrial-grade software.Fol...

Built with a rugged design and clear display, the TACNAV UMD offers: Highlights Active dot-matrix design, delivering unparalleled flexibility User-friendly interface with easy-to-read icons, messages, and pop-up menus Features Generation III NVG (night vision goggle)-compatible Four “soft keys” for easy operation Interchangeable with both Commander’s and Driver’s Displays, reducing logistics and cost Military standard approved for outstanding performance and reliability Ideal for integration into digital Battle Management Systems Compatible with all existing and future EMCORE TACNAV systems Applications Military vehicle requiring a user-friendly interface for its tactical navigation system The TACNAV UMD is controlled by the Arms Export Control Act (Title 22, USC Sec 2751 et seq.) and the International Traffic in Arms Regulations, ITAR 22 CFR 120-130, and may not be exported from the United States or disclosed to a foreign person in the United States except as authorized by those regulations.

It is commonly used in industrial and other devices to generate triggers ranging from one to several thousand FPS, ensuring precise timing synchronization with various devices. Periodic Mode: Continuously generates trigger signals after configuration. Burst Mode: Generates a single trigger signal upon receiving the best command via serial communication. *** Product Expansion and Usage ***  Four Operating Modes  Periodic mode: Generates a single-cycle signal based on the configured frequency and duty ratio.  Burst mode: Generates a single-cycle signal synchronized with a software trigger.  External trigger mode: Generates a single-cycle signal synchronized with an external trigger.  External trigger bypass mode: Distributes signals triggered externally.  Connect the trigger output signals from a Master Trigger Generator to a Slave Trigger Generator (as shown below).  By connecting one of the Master TG’s Trigger Outputs (1 to 16) to the Slave TG’s External Trigger Input: Outputs 1 to 15 of the Master TG remain unchanged. Outputs 16 to 31 of the Slave TG will mirror the Master TG’s Trigger Output. (Note: Each trigger signal passing through a TG experiences a delay of ten ns. However, since trigger outputs operate in the range of tens to thousands of Hz, users will not notice the delay).  Example with 17 TGen-16C units: Produces up to 256 Trigger Output Channels (16 × 16).

Primarily used in medium-sized and large satellites, it provides high torque performance and momentum conservation. By localizing the Control Moment Gyro controller, which had previously been imported for Korea’s domestic satellite industry, Lumir has gained a competitive advantage in both performance and cost.

For : Elevator Assembly Tool A320 Project 3.5m (L) x 1.5m (W) x 2m (H )

- A red light mounted on the left side of the aircraft to indicate the aircraft's location - A green light mounted on the right side of the aircraft to indicate the aircraft's location - These lights indicate the aircraft's position, flight direction, and attitude - Visible/IR Mode, Steady/Flash Mode - Light Intensity : FAA FAR 29.1391 ~ 29.1395 - SAE ARP 5825A