Process for powering a jet or rocket engine with water by simultaneously separating hydrogen from oxygen and igniting the hydrogen in the combustion/compression chamber

Abstract

An improved method of powering a Jet or Rocket engine using water as a fuel by separating the hydrogen and oxygen and igniting the hydrogen with high voltage high amperage electricity in the compression/combustion chamber of the engine.

I claim: 
     
         1 . A method for fueling a jet or rocket engine with water comprising;
 A. Generating high voltage, high amperage electrical current,   B. Conveying said current into the compression combustion chamber of said engine via two or more conductors,   C. Arcing said current across the electrode tips of a multitude of opposing electrode pairs inside said chamber of said engine forming an arc array,   D. Conveying water from a temperature controlled holding tank into said chamber,   E. Spraying said water into said arc array with one or more spray nozzles and   F, Igniting said water with said high voltage high amperage arc causing a rapid expansion of gas volume resulting in thrust.   
     
     
         2 . An apparatus for fueling a jet engine or rocket engine with water comprising;
 A. A high voltage high amperage generator electrically connected to,   B. One or more high voltage high amperage capacitors or condensers electrically connected to,   C. A pair of rigid metal conductors inside a compression combustion chamber each having a plurality of electrode tips mirroring its polar opposite with equal air gap spacing to form a multiple electric arc,   D. A temperature controlled water tank holding water with,   E. A conduit means for conveying said water to,   F. One or more water spray nozzles located inside said chamber to focus water spray into said electric arc.