Abstract: This invention relates to a nuclear fusion reaction process utilizing a B-11 isotope ion spherical plasma. Said spherical plasma will be formed on roof of a ferromagnetic chromium steel hulled aircraft, utilizing two larger magnesium based aircraft. Said spherical plasma is formed by raising a pyramid shaped device with a slotted glass ball electrode on top, on roofs of said air-craft. Only the smaller craft will utilize the fusion fuels, B-11 isotope ion and H-1 atom, in forming said spherical plasmas. The two larger craft will apply pressure toward smaller craft, and coalesce their plasmas into the smaller plasma. By forming this induced magnetic field, an electron current existing in larger applied magnetic field, is raised to middle of smaller aircraft spherical plasma. Ignition can be accomplished with land based neutral beam, FIG. 15. Produced energetic charged particles, electric energy, can be stored within craft plasma vortices and beamed to power stations.

Abstract: The invention relates to an electrolysis system. Said system can be utilized in a nuclear fusion process, on roof of a ferromagnetic aircraft in preferred embodiment. Said electrolysis system will utilize electric energy produced by said aircraft at no cost. Said energy will be provided to an array of electrodes to electrolyze water or seawater to produce protons and electrons, and with B-11 isotope ions, vaporized out of source on board craft, a fusion spherical plasma can be produced on roof of said aircraft, for a nuclear fusion reaction. Stored energy produced by electrolysis system, can also be used for other purposes. Said fusion spherical plasma is produced at essentially no cost, other than cost of electrolysis system and aircraft. Three aircraft will be utilized in preferred embodiment, all three craft utilizing an electrolysis system, though only one craft, the ferromagnetic craft alone, producing the B-11 isotope ion.

Abstract: The invention relates to a plasma based aircraft maintained in a flight mode by rotating plasma vortices located above and beneath said aircraft. Said aircraft is comprised of chromium steel, or higher ferrochromium steel can be used. Said aircraft receives energy from aircraft produced plasma obtained from the atmosphere. Produced energy is stored within craft oscillatory circuit and plasma vortices. When energy from craft capacitance system is depleting, energy can be obtained from craft inductance system from craft magnetic field. Said craft is capable of space flight, use as a submersible craft, boring device, or lifting device. Particle propulsion in space will be accomplished utilizing metal ions stored within craft capacitor plates. Said craft is opaque to electromagnetic radiation, and also absorbs radiation directed at craft. Said craft is capable of verticle ascent, descent and landing, and is lenticular in shape. Said aircraft can operate within earth radiation belts safely.

Abstract: This invention relates to a plasma gun utilized in a plasma based aircraft maintained in a flight mode by rotating plasma vortices located above and beneath said aircraft. Plasma produced by aircraft is utilized by said plasma gun to facilitate initial take off of craft, and also to accelerate aircraft speed, or, within an emergency, as needed. Said aircraft can also eject plasma through aircraft central shaft or within any direction from sides of said craft, for escape, evasion or normal accelerated flight. Preferred embodiment for said plasma gun, is a coaxial plasma gun, utilizing the large capacitance potential of aircraft, the large supply of aircraft produced plasma off said capacitors, or from uninsulated conducting wires, and also utilizing the strong Lorentz force existing within craft. The plasma produced by ionization within craft strong magnetic field, will enable this craft to rapidly avoid impediments to flight, or oncoming dangers.