Low-cost, high-performance start tracker for ultra-small satellites (such as CubeSats).
A low-cost, high-performance star tracker that can be used as a sensor for attitude control of ultra-small satellites (such as CubeSats) and small satellites. Additionally, there is a simulator available for evaluation during thermal vacuum testing.
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basic information
The main specifications of the nanoST (nanoStar Tracker) are as follows: FOV: 15° Accuracy: 40 arcsec (3σ) cross boresight; 200 arcsec (3σ) about boresight Maximum slew rate: 1°/sec Mass: 180g (with baffle for CubeSat); 220g (with baffle for non-CubeSat) Size: 90mm x 52mm x 38mm (for CubeSat); 118mm x 63mm x 63mm (for non-CubeSat) Voltage: 5V Power consumption: 1W Operating temperature range: -30 to +70℃ Communication protocol: UART Radiation tolerance: 20krad We can also provide a simulator for evaluation during the star tracker thermal vacuum test.
Price information
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Delivery Time
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Applications/Examples of results
A star tracker that can be used for various types of ultra-small artificial satellites. It has a proven flight record.
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The Advanced Technology Research Institute is an engineering company that supports space development and utilization, including rockets and artificial satellites, in Japan and around the world. We conduct a wide range of activities from the design and development of space systems, subsystems, and components for satellites and rockets, both small and large, to the sale of overseas space equipment. Additionally, we sell solar cells for space and ground use, and we design and develop solar cell panels for space as well as sell solar power generation modules and systems for ground use. For small satellites, including CubeSats, we provide system development from 1U to 12U, offer bus components, design and develop bus equipment, assemble satellites, and conduct integration and testing of satellites, including payloads. We also design, develop, and sell small electric propulsion systems for CubeSats and small satellites.