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We sell radiation-resistant cover glass for solar cells used in satellites and other applications. We can accommodate various sizes and thicknesses. AR coating is also available.
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A pulse plasma thruster (nanoPPT) that can be used as a propulsion device for ultra-small satellites. This propulsion device is compact, lightweight, and high-performance, suitable for applications such as satellite attitude control and orbit maintenance.
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A software transceiver that can be used for communication with low Earth orbit, medium Earth orbit, and geostationary satellites. This software radio uses the latest Xilinx Zynq SoC. It is a transceiver that allows for switching communication methods by changing the control software without modifying the hardware. It can also be used for inter-satellite communication and as a transponder.
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We provide an electric propulsion system using Hall thrusters that can be used as a propulsion device for artificial satellites and similar applications. The system includes a thruster, propellant tank, propellant supply system, and power control unit (PPU). It can operate with xenon or krypton as propellants.
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Image Processing Computer (IPC) for satellites using the highest possible Virtex 7 FPGA. Its features include the ability to process and store numerous complex images at speeds exceeding 30 Gbps by utilizing high-performance processors and memory functions. Additionally, this IPC has a track record of over 10 years of use in orbit.
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The solar sensor light simulator uses a light source stabilized and controlled by an optical ground support equipment (OGSE) to simulate optical sensors. This simulator can be used during thermal vacuum testing. Additionally, this simulator can be used without making contact with the sensor being simulated. The configuration of the simulator consists of a controller, three optical heads, and an interface to a PC. This simulator can be used with solar sensors, solar panels, and other optical devices from any manufacturer.
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Development and manufacturing of space shut-off valves (latch valves) are being carried out. Currently, three types of shut-off valves are being developed and manufactured. These valves can be used in propellant supply systems for both chemical propulsion and electric propulsion. Other products include solenoid valves, among others.
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This is an ultra-small, lightweight, high-performance infrared Earth sensor for ultra-small satellites, CubeSats. The field of view (FOV) of this Earth sensor is 90° vertically and 80° horizontally, with an accuracy of less than 1° (3σ).
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This is a solar sensor for ultra-small, lightweight, high-performance CubeSats. This solar sensor uses a CMOS image sensor, with a field of view (FOV) of 166° and an accuracy of <0.2° (2σ).
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A ground support equipment (GSE) that can be used during thermal vacuum testing of a simple, robust, and low-cost star tracker for satellites. It accurately reproduces actual star patterns with a compact and stable controlled LED light source, ensuring reliability and reproducibility.
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Provision of radiation-resistant and fault-tolerant lithium-ion battery modules for satellites. Available in two types: 28V and 50V. Equipped with built-in overcurrent, overvoltage, low voltage protection functions, and heaters.
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By utilizing triple-junction GaAs solar cells with more than 1.5 times the conversion efficiency of conventional silicon-based solar cells, there are advantages in both efficiency and cost compared to traditional systems in large-capacity concentrated solar power systems.
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This is a radiation-resistant single-board computer developed for space use, of course, for satellites and rockets. This computer significantly increases processing speed compared to conventional ones due to its use of commercial electronic components, and it can be offered at a lower price than traditional space components because it utilizes these commercial electronic parts. Furthermore, all the commercial electronic components used have been selected and tested by Space Commercial Parts to ensure they can be used for space applications.
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Flexible high-efficiency crystalline silicon solar cells and high-efficiency triple-junction GaAs solar cells are utilized in numerous spacecraft such as artificial satellites. Solar panels using these solar cells are also provided. Additionally, flexible GaAs solar cells for space applications are also available.
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A low-cost, high-performance star tracker that can be used as an attitude control sensor for ultra-small satellites (CubeSats). Its features include the use of commercial electronic devices, allowing for higher performance electronics compared to conventional space star trackers, and a radiation-resistant design.
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Free membership registrationWe will develop a small satellite system with a proven track record of low-cost launches that meets mission requirements (observation, communication, science, etc.).
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