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.

Specification Array Format : 1280 × 1024 Pixel pitch : 10㎛ Spectral range : 0.9㎛ ~ 1.7㎛ (SWIR) Operability : ≥ 99.5% Quantum Efficiency : 70% @ 1550nm Application Near-infrared Imaging Imaging Spectroscopy Surveillance Medical Science and Biology Astronomy and Scientific Material inspection Food inspection Forgery detection

Threaded bushing enables localized reinforcement of and attachment to panel structure. Supplied with disposable installation fixture. 1.25" Flange Diameter. SIZES: Imperial fine thread sizes from 10-32 (.190"-32) to 3/8-24 (.375"-24), Imperial coarse thread sizes from 8-32 (.164"-32) to 3/8-16 (.375"-16), and metric thread sizes from M5 to M8. 1.25" Flange Diameter. Grip lengths from 0.25" to 1.50". MATERIALS: Aluminum, 300 Series Stainless Steel, A-286 Stainless Steel, 316 Stainless Steel, and Titanium. Optional epoxy primer. FEATURES: Standard 1.25" diameter flange, 0.75" x 1.25" trimmed flange optional.

• Threaded, bayonet or push-pull coupling connectors • Mil spec series • Coaxial connectors • Power connectors • F/O & data connectors

Leveraging industry’s leading MEMS technology to provide previously unheard of capabilities in angle random walk values (0.02°/√hr.) without loss of tactical grade levels across military environments, including 1°/hr. bias stability, the SDI500 is designed to achieve the demanding performance levels required in sophisticated systems applications. It is particularly suited for use by Integrators and OEMs, packaged in a highly miniaturized, cylindrical configuration with a volume of only 19 cubic inches. Boasting a 20-Year lifetime capability without requiring calibration and a MTBF of more than 100,000 hours, multiple output data formats and SDLC, RS232 and UART output interfaces are provided in this revolutionary IMU for optimized systems protocols.

Receives vibration signals from an accelerometer installed on the aircraft engine and monitors engine vibration. Processes real-time vibration signals and converts them into IPS AVG units for output. Developed for localization, achieving 50% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x2 UART(RS-422/485) - x2 Accelerometer sensor - Sample rate : Up to 5,000Hz - Size : 220 x 206 x 52 (mm) - Weight : 1.75Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 10W)

Product Assurance Consulting : 1. The recent paradigm shift in newspace has expanded opportunities for new companies to enter the space industry. 2. Space product warranties pose a barrier to new entrants into the space industry. 3. MID has developed various programs to provide product warranty consulting services to new entrants to the space industry and offer customized services to our clients.

0.8m급 고해상도 초소형 지구관측 위성으로, 군집운용을 통해 고빈도 · 정밀 감시체계를 구축합니다. SpaceEye-M is a small satellite to produce high-resolution image data. A constellation of SpaceEye-M can perform precise monitoring over a large area with high revisit.