Business Areas

We have participated in national defense projects for the development of fire support, rapid assault, surveillance, and reconnaissance systems,
contributing to reinforcing the nation's defense capabilities. < The Government Order on National Security and Military Forces Development Projects >

Precision Guided Munitions

We deliver diverse tactical and cruise missiles based on our core technologies
in all types of guided munitions ranging from seekers to
warheads/fuzes, guidance and control systems, and propellants.

Product Information

  • 230MM-CLASS MULTIPLE ROCKET LAUNCHER, 'CHUNMOO'

    230MM-CLASS MULTIPLE ROCKET LAUNCHER, 'CHUNMOO'

    We developed a 230mm-class multiple rocket launching system ("MRLS"), Chunmoo, as a prime contractor. Chunmoo, an improved version of the existing MRLS rockets, is capable of firing different types of rockets depending on the intended target, remaining the key component of the nation's artillery systems. GPS/INS-guided munitions provide long-range, precision-strike capabilities, enabling precision strikes fired from outside the range of the enemy's long-range missile defense system.

  • LONG RANGE SURFACE-TO-AIR MISSILE

    LONG RANGE SURFACE-TO-AIR MISSILE

    As a critical part of the Korean Air and Missile Defense (KAMD) system, our long range surface-to-air missile is a guided exoatmospheric, hit-to-kill missile which collides with an incoming warhead during its final trajectory at an altitude of 40km or above.

  • TACTICAL SURFACE-TO-SURFACE MISSILE

    TACTICAL SURFACE-TO-SURFACE MISSILE

    This is a ballistic missile developed for tactical purposes.

  • LIGHT ARMED HELICOPTER AIR-TO-SURFACE MISSILE

    LIGHT ARMED HELICOPTER AIR-TO-SURFACE MISSILE

    Designed to be mounted on the nation's light armed helicopters, this air-to-surface missile is used to strike armor units such as tanks and mechanized infantry.

Core technology

We have developed the following core technologies that enable precision-strike capabilities.

  • SEMI-ACTIVE LASER SEEKER

    SEMI-ACTIVE LASER SEEKER

    This seeker utilizes a laser sensor to detect a target and marks the target for a guided weapon.

  • LASER DESIGNATOR & RANGE FINDER

    LASER DESIGNATOR & RANGE FINDER

    This laser light-based equipment measures distance to a target and designates it. It can be mounted on ground launch vehicles, helicopters, assault aircrafts, and unmanned systems.

  • IIR/CCD DUAL-MODE SEEKER

    IIR/CCD DUAL-MODE SEEKER

    Using ultraviolet and infrared imaging, this seeker enhances terminal guidance performance and is suitable for mid and long-range guided munitions.

  • DIRECTIONAL WARHEAD

    DIRECTIONAL WARHEAD

    Developed for guided anti-ballistic munitions, this warhead attacks the enemy's guided missiles by creating fragmentation charges and dispersing the missiles' penetrators when it reaches close proximity.

  • FUSE, GUIDED MISSILE

    FUZE, GUIDED MISSILE

    Electronic Safe Arm Fuze is impact or impact-delay type for guided missile.
    *ESAF : (Electronic Safe Arm Fuze)

  • GUIDANCE & CONTROL SYSTEM

    GUIDANCE & CONTROL SYSTEM

    This system produces control signals to direct flight control based on target information obtained from a seeker.

  • NAVIGATION SYSTEM BASED ON MICRO ELECTRO MECHANICAL SYSTEM

    NAVIGATION SYSTEM BASED ON
    MICRO ELECTRO MECHANICAL SYSTEM

    As a high-impact resistant navigation system that combines an inertial sensor built with a micro electro mechanical system (MEMS) and a multi-mode GPS receiver, this system is used for various tactical weapons and artillery ammunitions.

  • INERTIAL NAVIGATION SYSTEM BASED ON RING LASER GYROSCOPE

    INERTIAL NAVIGATION SYSTEM BASED ON RING LASER GYROSCOPE

    This inertial navigation system based on a ring laser gyroscope is used for a wide spectrum of weapon systems ranging from guided munitions aircrafts, naval vessels, and vehicle weapon control systems.

  • DIVERT & ATTITUDE CONTROL SYSTEM

    DIVERT & ALTITUDE CONTROL SYSTEM

    As a propulsion system developed to support hit-to-kill interceptors, this system makes rapid corrections of their flight path and altitude adjustments.

  • DUAL-PULSE ROCKET MOTOR

    DUAL-PULSE ROCKET MOTOR

    This motor contains two propellant segments separated by a barrier insulator, each with its own igniter. Its energy efficiency enhances the average speed and terminal speed of guided missiles, helping improve their mobility and precision.

  • ACTUATOR

    ACTUATOR

    This actuator is a core component of guidance systems, which converts electric signals from a remote terminal into motion and directs a missile to a target.

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