GE Aviation and Safran launched on June 14, 2021, a bold technology development program targeting more than 20 percent lower fuel consumption and emissions c...

The ACTUS® ARKS5255 (5-25X, 56mm FFP) Long Range Riflescope is designed for precision and durability, meeting the needs of professional users across a wide range of environments. Equipped with a First Focal Plane (FFP) optical design, it enables fast and accurate target coverage at any magnification level. The illuminated reticle ensures smooth and clear targeting in low-light conditions, such as during dawn or dusk. Whether in challenging operational environments or critical moments, the ACTUS® ARKS5255 is the ideal riflescope for users seeking superior performance when it matters most.

The main wheel assembly refers to the complete structural unit that includes the wheel, tire, axle, bearings, and in most cases, the braking system. As the primary load-bearing gear, the assembly is engineered to absorb high-impact forces during landing and provide strong braking performance during deceleration. Its design integrates durability, safety, and serviceability, making it a critical element of aircraft ground operations.

The SCVPX-SSGM (Synchronous Signal Generation Module) generates synchronization signals to coordinate the operation and timing of various radar system components. It can generate synchronization signals using an internal clock, receive an external clock, or regenerate synchronization signals from external sources to maintain precise timing cycles. A device driver program is required for configuration and operation, and the Linux driver can be downloaded from Seedcore’s product page. Drivers for other operating systems can be developed upon request. This module is deployed in the L-SAM multi-function radar system, providing precise timing synchronization across mission-critical subsystems.

Lumir is the first Korean company to successfully develop and manufacture this onboard equipment, delivering superior performance and significant cost savings compared to competitors’ products. By integrating non-volatile NAND flash devices into the image data handling unit, storage capacity has been significantly increased, with data retention maintained even when the power is off.The image data handling unit of the satellite is a core device that receives high-speed, large-capacity data output from Earth observation sensors mounted on the satellite—such as SAR or optical cameras—then compresses and stores the data in real time, while also performing encryption and encoding for transmission to ground stations. Lumir has successfully developed and manufactured this satellite-mounted device domestically in Korea for the first time, breaking reliance on imported technologies. This achievement secures Lumir’s competitiveness by delivering superior performance and significant cost savings compared to foreign products.

< Frequency Range > ● LB-400: 400 ~ 460MHz ● LB-900: 800~928MHz ● MB-1500: 1300~1500MHz ● MB-2400: 2400 ~ 2500MHz ● HB-5.2: 5150 ~ 5250MHz ● HB-5.8: 5725 ~ 5875MHz < TX path output Power (at antenna port) > ● Normal mode: 35dBm [min] ● On each antenna port 2x 35dBm ● Interference mode: 40dBm [min] < TX path maximum Input Power > ● +20 dBm < RX path Gain > ● 25dB typ. < RX path Noise figure > ● Low bands: 3dB max. ● High bands 3.5dB max. < RX path IIP3 > ● -10dBm typ. < RX IP1dB compression point > ● 15dBm typ. < Power Supply > ● +24V ± 1 Vdc

It is especially suited for demanding applications, which require reliable performance, such as missile seeker gimbal stabilization, where small size and low power consumption is required, while in a low cost design that is also ideally suited for high volume commercial applications. System Performance PARAMETERS SPECIFICATIONS Standard Ranges ±100°/sec, ±200°/sec, ±400°/sec Input Voltage + and - 5.0 Vdc Bandwidth 110 Hz Output Noise < 005°/sec/√Hz Scale Factor Accuracy ±1% Nominal Features Dual Axis Capabilities in Small Form Factor Miniature Size: Only 25gm.(1.05” x 0.71” diameter) Hermetically Sealed In Stainless Steel Cylinder High Reliability DC Input/High-Level DC Analog Output Low Cost Applications Tank Turret Stabilization Missile Targeting Platform Stabilization Antenna Stabilization Camera Stabilization Spacecraft

Shell : Silicone Rubber(Black) solderless terminal : KS D 5202, C5210R1/2H Rope : Nylon code(Black) Terminal : STS304(Black)