Ion plasma reaction drive

Abstract

An ion plasma reaction (IPR) drive system is disclosed which generates thrust by directionally accelerating relativistic velocity ion plasmas through closed loop magnetic confinement rings in order to interact more strongly with space-time. The IPR drive system provides an approach for the generation of continuous space vehicle acceleration without the need to eject on-board stored propellant. Charged particles are accelerated through a closed loop system up to velocities approaching the speed of light in such a manner that they strongly interact in an asymmetrical manner with space-time to generate continuous space vehicle acceleration. The supplemental means for electrical power generation and propulsive thrust augmentation are also disclosed.

What is claimed is: 
     
         1 . An ion plasma reaction (IPR) energy generation system, comprising:
 a magnetic containment ring;   an ion generation and injection system coupled to the magnetic containment ring and configured to generate streams of ionic particles into the magnetic containment ring;   a magnetic compression system in a first section of the magnetic containment ring; and   an ion acceleration system coupled to the magnetic compression system configured to accelerate the streams of ionic particles through the first section of the magnetic containment ring at a velocity faster than other sections of the magnetic containment ring and then through the magnetic compression system to generate an output of nuclear reactions as a power source.   
     
     
         2 . The IPR energy generation system of  claim 1 , wherein the ionic particle streams generated by the ion generation and injection system include a proton ion beam and an ion plasma stream. 
     
     
         3 . The IPR energy generation system of  claim 2 , wherein the proton ion beam is compressed between the ion plasma streams in the magnetic compression system. 
     
     
         4 . The IPR energy generation system of  claim 1 , further comprising a magnetic valve controlled to release the output of nuclear reactions from the ion acceleration system through a magnetic nozzle. 
     
     
         5 . The IPR energy generation system of  claim 1 , further comprising a charged particle source feeding charged particles into the ion generation and injection system. 
     
     
         6 . The IPR energy generation system of  claim 5 , wherein the charged particles are selected from protons, electrons, or ions. 
     
     
         7 . A space vehicle, comprising:
 a vehicle hull; and   an ion plasma reaction (IPR) drive system coupled to the vehicle hull to propel the space vehicle through space, the IPR drive system comprising,   a magnetic containment ring;   an ion generation and injection system coupled to the magnetic containment ring and configured to generate streams of ionic particles into the magnetic containment ring;   a magnetic compression system in a first section of the magnetic containment ring; and   an ion acceleration system coupled to the magnetic compression system configured to accelerate the streams of ionic particles through the first section of the magnetic containment ring at a velocity faster than other sections of the magnetic containment ring to generate an output of nuclear reactions as a supplemental electrical power source for the space vehicle.   
     
     
         8 . The space vehicle of  claim 7 , further comprising a magnetic valve controlled to release the output of nuclear reactions from the ion acceleration system through a magnetic nozzle. 
     
     
         9 . The space vehicle of  claim 7 , wherein the ionic particle streams generated by the ion generation and injection system include a proton ion beam and an ion plasma stream. 
     
     
         10 . The space vehicle of  claim 8 , wherein the proton ion beam is compressed between the ion plasma streams in the magnetic compression system. 
     
     
         11 . The space vehicle of  claim 7 , further comprising a charged particle source feeding charged particles into the ion generation and injection system. 
     
     
         12 . The space vehicle of  claim 11 , wherein the charged particles are selected from protons, electrons, or ions.