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We have demonstrated a complete thruster system that fits well within the body of a 10 cm cube cubesat configuration. This system uses a positive expulsion blowdown system to feed hydrogen peroxide to four thrusters around the base of the vehicle. The image below shows the system.
This system could be adapted to other configurations such as spacecraft with larger internal volumes and requirements for more thrusters and a larger propellant need. Below is a mass table for this system configuration.
We can assist in designing and integrating off-the-shelf tank systems into a variety of propulsion system designs. These include developing multi-structural elements for cubesats that use tanks as part of the structural element.
Thrusters sometimes have to oriented in triads or other multiple configurations. Our engineers can work with your team to design triads for a variety of spacecraft configurations. We also have pluggable thruster modules that can be readily integrated into rapid response spacecraft systems.
Whether you require a complete propulsion design or simple a thrusters assembly we can provide custom solutions to integrate into your specific application. Our system designs and concepts are flexible and adaptable to a variety of configurations.
We have experience recommending a variety of valve systems depending upon customer requirements and applications. Our thrusters are not tied to a single valve design allowing flexibility.