Rocket and satellite orbit and attitude control using hydrogen peroxide/kerosene engine. The feature is the use of environmentally friendly hydrogen peroxide as the oxidizer.
This is an engine that uses environmentally friendly hydrogen peroxide and kerosene as propellants for the orbital and attitude control of rockets and artificial satellites. Currently, there are two thrust levels available: 1,200N and 2,500N. In addition to the above, there are also engines and thrusters that use other bipropellant systems.
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basic information
The main specifications of the kerosene engine using hydrogen peroxide (90% wt) in space are as follows: 1. 1,200N Engine - Combustion chamber pressure: 2 MPa - Mixture ratio: 7.2 - Specific impulse: 280 sec - Operating voltage: 28±4 Vdc 2. 2,500N Engine - Combustion chamber pressure: 2 MPa - Mixture ratio: 7.2 - Specific impulse: 290 sec - Operating voltage: 28±4 Vdc
Price information
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Delivery Time
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Applications/Examples of results
The certification test for space use has been completed. It is currently being manufactured as a rocket engine.
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.