U.S. Patent No. 11952967B2 – Liquid propellant injector for vortex hybrid rocket motor
Various embodiments of a vortex hybrid motor are described herein. In some embodiments, the vortex hybrid motor may include a housing with a solid propellant positioned within the housing, and an injector ring positioned at a proximal end of the housing. Continue Reading U.S. Patent No. 11952967B2 – Liquid propellant injector for vortex hybrid rocket motor