Tri-Constituent Propellant Prototype Design and Build

Micro Aerospace has worked on the development of the tri-constituent propellant propulsion system from concept through prototype. This has included the specification, design, build and test of the thruster system utilizing an innovative catalyst design never used before in space. In less than two years MAS has taken this system design from concept to ready for spaceflight validation. This is relatively unheard of for a space-based propulsion system.