By supplying the highest level of products and services based on careful quality control management, our products have been recognized by various customers.

Features & Benefits: Drop-in enhancement for the T55-714A with very minor aircraft changes for deployment facility. Responsive to U.S. Army maintainer feedback, converting on lessons from current CH-47 engine. Upgrade Kit easily installed during overhaul.

With an AS9120-certified logistics system and strong semiconductor expertise, we are tailored to support defense and aerospace customers, where small-volume, high-mix requirements, long life cycles, and unpredictable demand are common. Beyond semiconductor components, we also provide electronic instruments and software solutions, serving as a total solution provider.

CI Systems사의 는 구성 가능한 소형 휴대용 미사일 방사 시뮬레이션 플랫폼입니다. MSS는 항공기 이륙 라인에서 정기 검사로 또는 실험실에서 미사일 경보 시스템(MWS)의 준비 상태와 성능을 테스트할 수 있도록 합니다. MSS는 자외선(UV) 또는 적외선(IR) 대역의 소형 방사 소스를 내장하고 있으며, 단일 또는 이중 방사 소스를 지원합니다. 이 소스는 내장된 마이크로프로세서에 의해 모드 조절되어 어떤 미사일이 방출하는 방사라도 현실적인 시뮬레이션을 제공할 수 있습니다. 사용자 친화적인 소프트웨어를 통해 어떤 테스트 프로파일도 MSS에 구성하고 업로드할 수 있습니다. Translated with DeepL.com (free version)CI Systems’ Missile Signal Simulator (MSS) is a configurable compact, hand-held, missile radiation simulation platform. The MSS enables the operator to test the readiness and performance of Missile Warning Systems (MWS) in the flight line as a routine test and in the laboratory. The MSS contains a miniature radiation source in the UV or IR band, with single or dual radiation sources. They are modulated by a built-in microprocessor capable of delivering a realistic simulation of the radiation emitted by any missile. Any testing profile can be configured and uploaded onto the MSS using a user-friendly software.

EMCORE’s IPADS-I (International) provides significant enhancements for today’s Army and Marine Corps survey teams. IPADS offers a proven, reliable, lightweight, off-the-shelf solution developed around four main components. > Compact Position/Navigation Unit (CPNU) > Control and Display Unit (CDU) > Battery and Charger Unit (BCU) > Porro Prism Assembly (PPA) All components are housed in a robust frame that allows for easy component access and stability, while facilitating a ready, two-person transfer between vehicles and aircraft. Features High-precision common survey enables efficient mass fires Impervious to jamming (inertial mode) Embedded Selective Availability Anti-Spoofing Module (SAASM) GPS option Navigation aids (compass rose and digital maps) In-vehicle and offset survey Combat-proven Embedded Built-In Test (BIT) High reliability MTBF, low mean time to repair (MTTR) No periodic calibration required Applications Artillery Survey to Mark: Survey Control Point (SCP) position; used to initialize weapon systems Orienting Line (OL) position and azimuth; used to initialize and align artillery assets

- The 2nd generation mightyZAP series supporting dynamic speed & current control as well as position control along with position & current feedback - Built-in drive circuit, position sensor, 12mm diameter coreless DC motor and gear box - 27/40/53/90mm stroke option - Rated Load of 12N ~ 100N according to gear ratio for each stroke (Speed is inversely proportional to Rated Load, so the stronger the Rated Load, the slower the speed.) -Support RS-485 or TTL / PWM communication * TTL / PWM communication version operates by automatically recognizing the input TTL / PWM signal * When using PWM communication, only the position command is available without position feedback (For feedback feature, use TTL or RS-485 communication) Both MODBUS RTU and IR open protocols available (Default : IR Open protocol)

It is a product lineup that is proven in global markets and has world-class competitiveness. And it is being exported to more than 20 countries around the world.

Every year, we celebrate World Space Week in October to honor scientists' contributions to space research and inspire the next generation of innovators. Honeywell has been a part of every NASA human space mission since the late 1950s, when our flight-control systems were installed on the X-15 Rocket Plane (shown above in a photo of Neil Armstrong after a research flight in November 1959).