A small, low-cost electric propulsion device that can be used for CubeSats. A plasma thruster using solid iodine as propellant.
An electric propulsion device using a plasma thruster that can be used for CubeSat propulsion. The size is 1.5U and the propellant used is solid iodine.
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basic information
The basic performance of the propulsion device is as follows: 1. Propellant: Solid iodine 2. Power consumption: 18–20W 3. Thrust: 0.3–0.5 mN 4. Specific impulse: 500–800 sec 5. Propulsion efficiency: 15–16% 6. Mass: 3kg 7. Size: 1.5U
Price information
Please contact us for pricing.
Delivery Time
※Please contact us regarding the delivery date.
Applications/Examples of results
Currently under consideration for recruitment at various institutions.
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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