With more than 3,000 EO/IR sensors on order or delivered, the Star SAFIRE® series provides the longest range performance in its class.

The SC-DSPRTM, a Seedcore Co., Ltd representative product, is a backplane transmission module that performs the I/O function of the DSP282A. When the DSP282A board is plugged into the motherboard(Backplane) in front of the Chassis, you can extend the I/O function of the board by plugging the SC-DSPRTM board into the back of the Backplane. The DSP282A board consists of two computing nodes. To support this, Ethernet, USB, MMCX, and mini-HDMI ports are allocated to each node, and synchronization signal input ports can also be used simultaneously on both nodes.

To guarantee maximum safety and reliability, our DA 30 features a brushless motor and a contactless wear-free position sensor. This means maximum service life with the greatest‐possible power delivery and its design prevents electromagnetic emissions (EMI) caused by brush sparking. The housing made of saltwater‐resistant aluminum is HART‐coat treated, meets the IP‐67 standard for water and dust sealing and provides an integrated Sub‐D connector (MIL spec. circular connector or cable gland on request). Brackets integrated in the housing for horizontal and vertical assembly. 8‐fold, ball‐bearing supported, steel gear train, drive shaft with ANSI multi‐tooth. The DA 30 series can be equipped with a standard PWM input (Pulse Width Modulation) that has two different interfaces: a differential, galvanic isolated interface (Opto‐Coupler) and a single‐ended interface with CMOS levels that is also used to program the servo parameters. It includes analog position feedback to detect the drive shaft position. A differential RS‐422 PWM interface can be chosen instead of the opto‐coupled interface. The DA 30 with digital serial command interface (RS‐485) receives its commands via a CRC secured protocol. It can return not only the shaft position in digital format, but also several diagnostic data such as the level of the supply voltage, current consumption and the temperature of the motor and electronics in digital form (optionally also the humidity within the actuator case). These kind of diagnostic capabilities help to determine the health state of the actuators before, during and after deployment.

SAR satellites are designed for change detection and our unique Dwell, Spot, Strip and Scan modes give you the flexibility to monitor very large areas and zoom in to areas of interest at ultra-high resolution as needed. Get unprecedented visibility and flexibility with Dwell, Spot, Strip and Scan imaging modes. Monitor areas up to 50,000 km² and zoom in to areas of interest at very high resolution down to 50 cm – day, night and in any weather

RSAQ Series we designed is a series of Display Head Assembly Unit which is used in aeronautical instruments that meets the Air Transport Indicator (ATI) standard. Ruggedized Square TFT color LCD monitor is designed and tailored for use in harsh, demanding environments like Airborne application. RSAQ Series are 100% customized. Various types of ATI are available - LCD glass, LCD glass with T-con board and module with LED BLU

Plane Windows are used as substrates for a variety of applications, such as laser window, output couplers, beamsplitters, beam combiners, mirrors, dichroic filters and plate polarizers. Considerations in selecting window substrates include transmission range, absorption coefficient, incident laser power density and environmental factors such as pressure, temperature, moisture, abrasion and corrosion. Plane Windows listed under UV / VIS / NIR substrates are specified for applications involving coating wavelengths 193nm ≤ λ〈2.0 μm. Units for these substrates are given in mm. Plane Windows listed under IR substrates are specified for applications involving coating wavelengths λ≥ 2.0 μm. Units for these substrates are given in inches. Refer to the THIN FILM COATINGS section for information on coatings that can be applied to these substrates.

The engine is suitable for MALE AUVs. Available in pusher and tractor configurations. Digital interface for control and monitoring. Stable operation at high altitudes and high temperatures. Ability to run at cold temperatures below -30°C without preheating.

Main Fuel Control, Servovalve, Switches, Indicators, Starter Generator, Power Unit, Gas Turbine, Control Unit, Ice Detector, Blade, Advanced Flight Control Computer, Manifold Assembly, Main Battery, Ring Bearing, Power Supply, Motor, Sensors