A low-cost, small reaction wheel for space use that can be utilized for attitude control of ultra-small satellites, CubeSats, and small satellites.
We sell reaction wheels that can be used for three-axis attitude control of ultra-small satellites, CubeSats, and small satellites. Additionally, we offer one-axis momentum/reaction wheels that can be used for medium to large satellites.
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basic information
The main specifications of the reaction wheel are as follows: 1. CW0017 Maximum angular momentum: 1.77 mNms @ 6,000 rpm Maximum torque: 0.23 mNm Rotational speed: ±10,000 rpm Operating temperature range: -20 to +80℃ Mass: 60 g Dimensions: 28 x 26 x 28 mm Input voltage: 3.3 Vdc & 6.4 to 16.8 V Average power consumption: 0.18 W @ 2000 rpm Maximum power consumption: 0.85 W @ maximum torque Interface: UART, RS485, CAN (I2C available as an option) Radiation resistance: 24 kRad 2. CW0057 Maximum angular momentum: 5.7 mNms Maximum torque: 2 mNm Mass: 115 g Dimensions: 35 x 24 x 35 mm Average power consumption: 0.336 W @ 2000 rpm Maximum power consumption: 2.7 W @ maximum torque All other specifications are the same as CW0017 3. CW0162 Maximum angular momentum: 16.2 Nms Maximum torque: 7 mNm Mass: 144 g Dimensions: 46 x 24 x 46 mm Maximum power consumption: 7.2 W @ maximum torque All other specifications are the same as CW0057
Price information
Please contact us regarding the price.
Delivery Time
※Please contact us regarding the delivery date.
Applications/Examples of results
We have a lot of experience in attitude control for ultra-small satellites, CubeSats, and small satellites.
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Company information
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.
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