Sierra Space Corporation

Ryan C Cavitt

Christopher P St Clair

Patrick D Satyshur

Scott M Munson

Trevor P Ormonde

Jake W Carey

Various embodiments of a vortex thruster system is described herein that is configured to create at least three discrete thrust levels. In some embodiments, the vortex thruster system is configured to decompose a monopropellant and deliver the decomposed monopropellant into a vortex combustion chamber for generating various thrust levels. In some embodiments, the vortex thruster system includes a secondary propellant valve configured to deliver a secondary propellant into the vortex combustion chamber containing decomposed monopropellant to create a high thrust level. Related systems, methods, and articles of manufacture are also described.

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Waunakee, WI, United States of America

Ryan C Cavitt