Rocket motor propellant injection system

Claim 1

A FLUIDALLY CONTROLLED SYSTEM FOR INJECTING LIQUID PROPELLANT INTO THE COMBUSTION CHAMBER OF A ROCKET MOTOR, COMPRISING: A LIQUID PROPELLANT SUPPLY RESERVOIR; A FIRST WALL ATTACHMENT AMPLIFIER HAVING FIRST AND SECOND INLETS AND FIRST AND SECOND OUTLETS AND ARRANGED SO THAT SELECTIVE VARIATION OF THE VOLUME OF FLUID INJECTED INTO SAID SECOND INLET DIRECTS THE FLUID INJECTED INTO SAID FIRST INLET THROUGH SAID FIRST OUTLET ONLY, THROUGH SAID SECOND OUTLET ONLY, OR THROUGH BOTH SAID FIRST AND SECOND OUTLETS; A FIRST CONDUIT COMMUNICATIVELY CONNECTING SAID FIRST INLET OF SAID FIRST WALL ATTACHMENT AMPLIFIER WITH SAID LIQUID PROPELLANT SUPPLY RESERVOIR; A VORTEX AMPLIFIER HAVING A FIRST INLET THROUGH WHICH FLUID CAN BE INJECTED RADIALY INTO THE INTERIOR THEREOF, A SECOND INLET THROUGH WHICH FLUID CAN BE INJECTED TANGENTIALLY INTO THE INTERIOR THEREOF AND INTO IMPINGEMENT WITH FLUID INJECTED INTO SAID FIRST INLET, AND AN OUTLET; A SECOND CONDUIT COMMUNICATIVELY CONNECTING SAID FIRST INLET OF SAID VORTEX AMPLIFIER WITH SAID FIRST OUTLET OF SAID FIRST WALL ATTACHMENT AMPLIFIER; A THIR CONDUIT COMMUNICATIVELY CONNECTING SAID SECOND INLET OF SAID VORTEX AMPLIFIER WITH SAID SECOND OUTLET OF SAID FIRST WALL ATTACHMENT AMPLIFIER; A SECOND WALL ATTACHMENT AMPLIFIER HAVING FIRST AND SECOND INLETS AND FIRST AND SECOND OUTLETS AND ARRANGED SO THAT SELECTIVE VARIATION OF THE VOLUME OF FLUID INJECTED INTO SAID SECOND INLET DIRECTS FLUID INJECTED INTO SAID FIRST INLET THROUGH SAID FIRST OUTLET ONLY OR THROUGH SAID SECOND OUTLET ONLY; A FOURTH CONDUIT COMMUNICATIVELY CONNECTING SAID FIRST INLET OF SAID SECOND WALL ATTACHMENT AMPLIFIER WITH SAID OUTLET OF SAID VORTEX AMPLIFIER;