A device that integrates and displays comprehensive navigation information for submarines, enabling operators to control various navigation sensors and systems while supporting mission execution. - Compliant with MIL-SPEC standards (shock, vibration, temperature/humidity, EMI/EMC) - Mechanically engineered design for improved maintainability

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).

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)

STIM300 is a small, tactical grade, low weight, high performance non-GPS aided Inertial Measurement Unit. It contains 3 highly accurate MEMS gyros, 3 high stability accelerometers and 3 inclinometers. The IMU is factory calibrated and compensated over its entire operating temperature range. STIM300 is a cost-effective ITAR free solution for systems that only had FOGs as an alternative when reaching for the performance level of that STIM300 can offer. Each axis is factory calibrated for bias, sensitivity and compensated for temperature effects to provide high-accuracy measurements. The unit runs off a single +5V supply and communicates via a RS422 interface. The use of a 32-bit RISC ARM microcontroller provides flexibility in the configuration, like choice of output unit, sampling frequency, LP filter -3dB frequency and RS422 bit-rate and protocol parameters. For more advanced users, STIM277H may be put in Service Mode. In this mode all the configuration parameters can be temporarily or permanently changed by overwriting the current settings in the flash memory. Service Mode also provides the ability to perform single measurements, perform diagnostics and obtain a higher detail in the status byte.

EDS is applied high-power LED light source to achieve fast target acquisition of shooter. With an efficient LED light source, EDS guarantees more than 50,000 hrsof operation time (Continuous use). EDS allows for better situation awareness and fast target engagement especially from non-standard shooting position. EDS can be used for hunting/recreational purpose.

항공 엔진용 테스트셀·시험장비 및 데이터 솔루션을 설계·구축하는 세계적 기업으로, 상업·국방·MRO 고객의 터보팬/터보샤프트/APU 등 다양한 엔진 시험 요구를 지원합니다.

High-Density Space-grade NAND Flash memory : 1. Density : 128Gbit (2G x 8bit x 8chips) NAND Flash 2. Package Type : 54 Pin SOP (Small Outline Package) 3. Radiation : TID > 60 krad, SEL (TBD)

The KX1-3046 is an X-band high-power MMIC amplifier fabricated on the GaN-on-SiC process. It operates from 8.0 – 10.5 GHz and typically provides 30W saturated output power with power-added efficiency of 46%. The KX1-3046 can support military and commercial radar systems. It is matched to 50Ω with integrated DC blocking capacitors on both RF input and output ports. The KX1-3046 is 100% DC and RF tested on-wafer. It is available in chip form. **Key Features** - Frequency Range: 8.0-10.5GHz - Small Signal Gain: 28dB - High Pout: 30W - High PAE: 46% - DC bias: Vd=28V @Idq=0.6A - Pulsed Vg: PW=100µs, DC=10% - Chip size: 2.95x3.1x0.1mm