Colloid Thruster for Attitude Control Systems (ACS) and Tip-off Control Applications, Phase I

We propose to develop and test key technologies needed for an integrated, high thrust colloid thruster system with no moving parts, for spacecraft attitude control and tip-off rotation cancellation. Busek has already successfully demonstrated the use of porous substrates as planar emitters for colloid thrusters. In this proposal we will pursue enabling technologies for such a thruster, such as a passive feedsystem and an isolation membrane for separating the propellant in the reservoir from the thruster head prior to launch. Advancements to date suggest viable approaches for the development of a cost-effective, reliable, and flexible thruster configuration.

This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.