Rocket and satellite attitude control thruster using hydrogen peroxide. The feature is the use of environmentally friendly hydrogen peroxide as the propellant.
This is a thruster that uses environmentally friendly hydrogen peroxide as a propellant for attitude control of rockets and artificial satellites. Currently, there are four thrust levels available: 1N, 50N, 100N, and 250N. Additionally, there are thrusters that use other environmentally friendly propellants (green propellants, ADN) besides those mentioned above.
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basic information
The main specifications of the space hydrogen peroxide (90% wt) thruster are as follows: 1. 50N Thruster - Combustion chamber pressure: 1.8 MPa - Specific impulse: 170 sec - Area ratio: 60 (in vacuum) - Operating voltage: 28±4 Vdc - Mass: 0.5 kg 2. 100N Thruster - Combustion chamber pressure: 1.8 MPa - Specific impulse: 170 sec - Operating voltage: 28±4 Vdc - Mass: 0.6 kg 3. 250N Thruster - Mass: 0.8 kg All other specifications are the same as the 100N thruster. 4. 1N Thruster - Maximum operating pressure: 2.4 MPa - Specific impulse: ≧140–167 sec - Minimum impulse bit: ≦0.1 Ns - Operating voltage: 24–32 V - There is also a thruster that uses 95% wt hydrogen peroxide.
Price information
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Delivery Time
※Please contact us regarding the delivery date.
Applications/Examples of results
The 50N thruster has a flight record for use in rockets. Additionally, the 100N/250N thrusters have completed certification tests and are being used for rocket control. The 1N thruster is under development for satellite use.
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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