Abstract: Integrated circuit (IC) packages are disclosed. In some embodiments, an IC package includes a glass substrate, a micro light emitting diode (LED), a semiconductor die, one or more through glass vias (TGVs) and a package substrate. The micro LED is positioned over the glass substrate. The TGVs are integrated into the glass substrate and connect the micro LED to the semiconductor die. The semiconductor die is connected to the package substrate to receive external signals when connected to a motherboard.

Abstract: A moon/planet complex, an orbiting docking spaceport, and transportation vehicles therebetween that includes i) moon/planet base station having a landing platform with a plurality of charged plates; ii) a moon/planet orbiting craft, docking spacecraft having landing platform with a plurality of charged plates; iii) a personnel transport spacecraft to shuttle personnel between an orbiting craft and planetary/moon base station having rotating electromagnetic rings 320 and/or rotating electromagnetic plates to interact with charged plates; iv) a large personnel/cargo transport spacecraft to shuttle personnel between an orbiting craft and planetary base station having rotating electromagnetic plates to interact with charged plates.

Abstract: A moon/planet complex, an orbiting docking spaceport, and transportation vehicles therebetween that includes i) moon/planet base station having a landing platform with a plurality of charged plates; ii) a moon/planet orbiting craft, docking spacecraft having landing platform with a plurality of charged plates; iii) a personnel transport spacecraft to shuttle personnel between an orbiting craft and planetary/moon base station having rotating electromagnetic rings 320 and/or rotating electromagnetic plates to interact with charged plates; iv) a large personnel/cargo transport spacecraft to shuttle personnel between an orbiting craft and planetary base station having rotating electromagnetic plates to interact with charged plates.

Abstract: A hypersonic harmonic exciter system to enable hypersonic speed, including a hypersonic harmonic exciter body having a plurality angled sides forming exciter body hollow structure with an access aperture, vibration inducing wave apparatus configured to produce and project vibration harmonic waves that converge on a convergence harmonic point forward of the hypersonic harmonic exciter body, the vibration inducing wave apparatus having vibration apparatus hollow structure with a series of exterior concentrically positioned vibration inducing bands, the vibration inducing wave apparatus inserted in the exciter body hollow structure, and harmonic sound projecting apparatus configured to produce and project harmonic sound waves that converge on the convergence harmonic point forward of the hypersonic harmonic exciter body, the harmonic sound projecting apparatus having sound apparatus hollow structure with a series of exterior concentrically positioned sound emitter bands, the harmonic sound projecting apparatus i

Abstract: A space based magnetic vortex accelerator and methods of use thereof having one or more sections of magnetic material configured as a conduit with a flightpath therethrough for the spacecraft, a magnetic coil field generator electrically connected to said one or more sections of magnetic material configured to generate a space based magnetic field via said one or more sections of magnetic material, a power plant electrically connected to said magnetic coil field generator, said power plant configured to power said magnetic coil field generator, one or more magnetic field receivers affixed to the spacecraft, said one or more magnetic field receivers configured to magnetically engage said space based magnetic field.

Abstract: A fire containment system strung across the ground and methods of use thereof, that generally includes two or more vertical towers anchored in series in the ground, a lift system integral to each of said two or more vertical towers having a plurality of vertically slidable swivel joints capable of vertical travel there up one of the two or more vertical towers, one or more cables, each cable strung between one of the plurality of vertically slidable swivel joints on each of the two of the or more vertical towers, a fire proof curtain affixed to said one or more cables, a below ground storage to contain said fire proof curtain.

Abstract: A space based magnetic vortex accelerator and methods of use thereof having one or more sections of magnetic material configured as a conduit with a flightpath therethrough for the spacecraft, a magnetic coil field generator electrically connected to said one or more sections of magnetic material configured to generate a space based magnetic field via said one or more sections of magnetic material, a power plant electrically connected to said magnetic coil field generator, said power plant configured to power said magnetic coil field generator, one or more magnetic field receivers affixed to the spacecraft, said one or more magnetic field receivers configured to magnetically engage said space based magnetic field.

Abstract: A fire containment system strung across the ground and methods of use thereof, that generally includes two or more vertical towers anchored in series in the ground, a lift system integral to each of said two or more vertical towers having a plurality of vertically slidable swivel joints capable of vertical travel there up one of the two or more vertical towers, one or more cables, each cable strung between one of the plurality of vertically slidable swivel joints on each of the two of the or more vertical towers, a fire proof curtain affixed to said one or more cables, a below ground storage to contain said fire proof curtain.