Temperature / Flame Resistant Seals Reinforced & Non-Reinforced Seals Vulcanized Bonding Custom Technical Elastomeric Solutions

The EPL4000, like the EPL2000, is an all-in-one RU/DU/EPC/application server system that provides seamless outdoor LTE service without backhaul connection. It offers a service radius of several kilometers and is optimized for installation inside ships and vehicles.

The Improved Fire Control System (IFCS) PNU / Universal Fire Control System (UFCS) UPNU family represents a true state-of-the-art system approach. Its design features permit ready adaptation and/or optimization to any current or future weapon system or sensor requiring precision pointing and positioning. The PNU / UPNU and its variants point the way for the future direction of the land navigation systems. Utilizing advanced sensors, electronics, software and aiding (GPS and odometer), the PNU / UPNU family delivers precisely what the Army of tomorrow needs — a system designed to remain operationally effective and affordable to support well into the future. Features High-performance RLG-34 ring laser gyros Common architecture and components (Paladin, PIM, Firefinder, IPADS) Embedded 12-channel Selective Availability Anti-Spoofing Module (SAASM) Impervious to jamming (inertial mode) Resistant to jamming (GPS-aided mode) Combat-proven Embedded Built-In Test (BIT) High reliability MTBF, low mean time to repair (MTTR) No periodic calibration required Applications Multiple Launch Rocket System (MLRS) High-Mobility Artillery Rocket System (HIMARS) Pointing and position location

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).

The S10s, the first model of the PabloM series, is a loitering munition designed for strike missions. Leveraging mesh communication and AI-enabled swarm flight, it can execute both simultaneous and sequential self-destructive strikes against targets, effectively neutralizing diverse “anti-drone” systems. The S10s launches autonomously from a dedicated platform and can sustain flight for over 30 minutes, enabling wide-area operational coverage. When engaging a target, it performs a steep dive of up to 45 degrees at speeds reaching 150 km/h, ensuring rapid and precise impact. Built from lightweight foam-board materials, the S10s is optimized for fast, large-scale production during operations. Furthermore, its modular open-architecture design, aligned with the K-MOSA concept, allows mission payloads to be quickly swapped and integrated, delivering exceptional flexibility and interoperability in real combat environments.

1. 용도 : 차량의 엔진동력을 이용하여 요구하는 전력을 생성하는 장치 2. 기능 : 정격출력 10kW, 3상 140V~560V 생성 3. 관련 장비/체계 분야 : 30밀리 자주대공포(비호복합), 단거리지대공무기(천마) 4. 관심 협업 분야 / 목표시장(국가) - 전차ㆍ장갑차 그 밖의 전투기동장비 / 국내 방위산업시장 및 해외 (미국, 멕시코, 프랑스, 이스라엘, 인도네시아, 말레이시아, 아랍에미리트, 유엔국 등) 5. 기타사항 - 영구자석 기반 발전기 기술 및 고효율 에너지변환 기술(특허보유) - 국방규격화 완료, 해외수출 경쟁력 제품

Introducing the FoldIR 30-450mm f/3.4 continuous zoom lens with Ophir's innovative folded optical design, offering lightweight, compact design while maintaining long optical lengths and improved tolerance sensitivity. This design ensures exceptional performance even in challenging environments, addressing stabilization and athermalization issues. Its unique f/3.4 aperture guarantees superior image quality, surpassing larger aperture zoom lenses in diffraction limit MTF and IR signal collection. The lens features a built-in mechanical shutter for NUC control, enhancing image quality through Ophir's control system. Weighting under 2kg, offering an impressive detection range of over 20km, and a horizontal field-of-view of 26.9º (WFOV) and 1.7º (NFOV). This compact, lightweight, long-range, high-performance lens is the ultimate selection of for optical air-land-sea optical gimbals and payloads. Key features include: • Efficient folded optics design for min. volume use • Physical shutter for NUC • Designed for MWIR 10μm SXGA sensors • For air-sea-land gimbals and payloads • Weight <2kg • Detection range >20km • HFOV 26.9º WFOV/ 1.7º NFOV

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.