About
Redefining Electric Propulsion
Focused on designing a cathodeless gridded ECR ion thruster that uses asymmetric pulsed neutralization to micro and minisatellites. It is designed for VLEO drag compensation and collision avoidance, prioritising efficiency and reliability.

Mission
Very Low Earth orbit will only get more prominent in the future as it offers less latency and unmatched surface resolution. It also is mostly self cleaning, meaning that it does not contribute to the Kessler Syndrome. VLEO though has significant atmospheric drag in comparison to a vacuum, meaning that any satellite requires an active propulsion system to not fall and burn up. So I am building that thruster, that is made to work best in VLEO, without requiring complex intakes like air breathing propulsion.


NEXT steps

CNC Machining of Thruster

Valve design and PiC simulation.

