A-29 SUPER TUCANO

EMCORE’s SDI170 IMU is designed as a performance-compatible inertial system that is form, fit, and functional with a legacy RLG-based IMU product, but with superior overall performance, versatility, and a significantly higher MTBF (Mean Time Before Failure) rating over ruggedized environments. The tactical performance of the SDI170 IMU is based on EMCORE’s mature, proven, dependable and accurate quartz MEMS inertial sensor technology in our SDI500 tactical-grade IMU. EMCORE’s quartz technology enables repeatable high-volume production of precisely machined sensor structures combined with the inherent large signal output and thermal stability of quartz materials. The SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.

The IMX-5™ includes Attitude Heading Reference System (AHRS) sensor fusion to estimate roll, pitch, and heading. Adding GNSS input to the IMX-5 enables onboard Inertial Navigation System (INS) sensor fusion for roll, pitch, heading, velocity, and position. Features Tactical Grade IMU Gyro: 1.5 °/hr Bias Instability, 0.16 °/√hr ARW Accel: 19 µg Bias Instability, 0.02 m/s/√hr VRW 0.04° Dynamic Roll/Pitch 0.13° Dynamic Heading Surface Mount Reflowable (PCB Module) Fast Integration with SDK and Example Software Data Logging (SDK and Application Software)

Engine Start Begins with ATS. The Air Turbine Starter (ATS) is a key component of an aircraft's secondary power system, driven by Bleed Air supplied from the Auxiliary Power Unit (APU) to accelerate the engine up to approximately 8,900 RPM, enabling engine start. Through the in-house development and localization of the ATS, we have incorporated power generation, optimal design of the shear section with consideration of failure, Containment functionality, as well as lubrication and power transmission systems. In addition, we have secured manufacturing and assembly technologies and continue development aimed at successful operation and the establishment of a mass production system.

· Cannon laying : Automatic/Semiautomatic /Manual(within 10 secon)ds · Elevation : 45 ~ 85°(driving speed 10°/sec) · Deflection angle : 360°infinite (driving speed 20°/sec) · Sighting Error : Max 3 mil(1σ) · Navigation System : Send location/orientation information

Companies of all sizes work with SC Commerce to develop and grow export markets throughout the world. Our presence in five foreign countries allows us to bui...

aviation fuel refueling cart : Mobile refueling cart that can easily refuel light aircraft and helicopters Sump recovery system : Collect the drained/sumped aviation fuel from the aviation fuel refueling system, easily sample and test it, and then decide whether to drain it or return it to the system. Aviation fuel refueling system : The aviation fuel refueling system is compactly constructed with a skid for easy use and installation.