Developed and manufactured by MPS Microsystems based on customer specifications, this lens actuator forms an essential component of a laser guidance system for unmanned flying objects. It enables 2 lens groups to be displaced individually over a total range of 48 mm and makes it possible to focus a laser over a distance of several kilometres. The main technical difficulty inherent to this actuator lies in meeting very stringent requirements for alignment between the two lens groups (< 10 µm) and in maintaining a very small tilt of the lenses over their entire stroke (lateral deviation < 2 µm). The key part making it possible to ensure such specifications is a frame machined by milling from an aluminium block, into which the 2 drive systems are fastened. These systems each consist of a Ø16 mm brushless motor and a Ø4 mm ball screw with an axial play of less than 5 µm. Backlash-free and frictionless sliding of the lens holders is ensured by standard L306 linear ball bearings manufactured by MPS Microsystems.

The mighty Hitec SG33BLT Series servo actuators operate on DroneCAN (formerly UAVCAN), CAN 2.0 A/B, RS485, PWM and TTL command protocols, and feature brushless motors, magnetic encoders, and hardened steel gears. They are also environmentally sealed with an IP67 waterproof case rating. The SG33BLT Series was initially developed for the automotive industry requiring minimal support equipment and wiring, saving unnecessary installation complexity, cost and weight. This same functionality is now enjoying widespread adoption of CAN and DroneCAN systems within the UAV environment. With options for both 9~15-volt and 18~32-volt operations, and DB9SUB, Circular, & Gland Cable connectivity, the SG33BLT Actuator Series is sure to have a solution for your needs. #UAV #UAS #UAM #UGV #UUV #USV

ALTERNATIVE TO M19648/1 SERIES

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.

The system can be used as a measurement device for first responders for the exploration of hazardous areas. GAMON-Drone system is designed to offer the best combination of portability, low power consumption and performance. The unit is assembled in a lightweight enclosure that contains both the Scintillator Detector and the Digital Signal Processing Electronics. GAMON-Drone can identify gamma-emitting radionuclides and differentiate them based on the category they belong to, distinguishing between NORM, medical and industrial.

1. 용도 : 전자제어기로부터 공급되는 전력으로 빠르게 가열하는 장치 2. 기능 : 8,200 Kcal/hr(차체 특성에 따른 난방효율 최적화 설계, 운용간 안정성 확보) 3. 관련 장비/체계 분야 : 30밀리 자주대공포(비호복합) 4. 관심 협업 분야 / 목표시장(국가) - 전차ㆍ장갑차 그 밖의 전투기동장비 / 국내 방위산업시장 및 해외 (미국, 멕시코, 프랑스, 이스라엘, 인도네시아, 말레이시아, 아랍에미리트, 유엔국 등) 5. 기타사 - 영구자석 기반 발전기 기술 및 고효율 에너지변환 기술(특허보유) - 국방규격화 완료, 해외수출 경쟁력 제품

Chelton’s vehicle intercom systems are engineered to provide exceptional communication clarity and security, even in the harshest operational environments. Designed with scalability and modularity at their core, they can be tailored to fit a wide range of vehicle platforms and mission requirements. Built to withstand extreme conditions, these systems ensure uninterrupted voice and data exchange, enabling teams to stay connected and effective in the most challenging scenarios. Backed by decades of expertise and trusted by defence forces worldwide, Chelton delivers robust, future-ready solutions that enhance situational awareness and mission success.

InterGravity Technologies has developed a Type-III Composite Overwrapped Pressure Vessel (COPV) optimized for high-performance small spacecraft propulsion systems. The tank is designed with an aluminum alloy liner for impermeability and a carbon fiber/epoxy composite overwrap for high strength-to-weight ratio. The system is tailored for green propellant storage (C₂H₆, N₂O), offering an exceptionally lightweight yet robust solution for orbital transfer vehicles and CubeSat-class platforms. Technical Specifications - Type : Type-III COPV (Al liner + CFRP wrap) - Volume : 5.3 liters - MEOP : 75 bar - Proof : 230 bar - Burst : 250 bar - Dry Mass : < 1.0 kg