István Lőrincz

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I am an entrepreneur with a strong passion for creating new opportunities and executing…

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Experience & Education

  • InternodeLAB

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Publications

  • Null-Results of a Superconducting Gravity-Impulse-Generator

    52nd AIAA/SAE/ASEE Joint Propulsion Conference, At Salt Lake City, UT

  • Design and First Measurements of a Superconducting Gravity-Impulse-Generator

    51st AIAA/SAE/ASEE Joint Propulsion Conference, Volume: AIAA 2015-4080

  • Replication and Experimental Characterization of the Wallace Dynamic Force Field Generator

    51st AIAA/SAE/ASEE Joint Propulsion Conference, Volume: AIAA 2015-4081

    In the 1970s, Henry W. Wallace filed a number of patents claiming that the rotation of masses with a net nuclear spin leads to the generation of a gravity-like force field that effects other rotating masses as well as heat conductivity. Based on his patent drawings we designed an experimental apparatus as close as possible to his original design including features to mount precision laser sensors to record speed and orientation of the rotating masses. It consists of a generator and a detector…

    In the 1970s, Henry W. Wallace filed a number of patents claiming that the rotation of masses with a net nuclear spin leads to the generation of a gravity-like force field that effects other rotating masses as well as heat conductivity. Based on his patent drawings we designed an experimental apparatus as close as possible to his original design including features to mount precision laser sensors to record speed and orientation of the rotating masses. It consists of a generator and a detector assembly with rotating masses as well as a massive top and bottom part of the same spin-polarizable material in order to provide an effective pathway for the claimed field.

  • Relevant Analysis of the Innovative Conrad Haas Manuscript From 1555

    History of Rocketry and Astronautics / American Astronautical Society

  • Extended Weight Measurements of Uncharged and Charged Spinning Gyroscopes in the Earth's Gravitational Field

    AIAA/ASME/SAE/ASEE Joint Propulsion Conference

  • Heavy plasma NAPALM propulsion simulation code

    International Congress on Computer Applications and Computational Science

  • Imaging Experiment On Board the Nerva-1 Rocket Vehicle

    Annals of DAAAM & Proceedings

  • Nanoparticle Accelerator with Lorentz Modulation

    International Astronautical Federation

    The new thruster will far exceed, by between ten and forty percent, the specific impulse in a vacuum of all existing electric and thermoelectric rocket engines. This will be accomplished through a new working medium, comprised of relatively high-mass nanoparticles that will be accelerated to very high kinetic energies. The best performing electric thrusters in the present are able to deliver up to 15.000s specific impulse, but the new thruster is expected to deliver between 18.000 and 30.000s…

    The new thruster will far exceed, by between ten and forty percent, the specific impulse in a vacuum of all existing electric and thermoelectric rocket engines. This will be accomplished through a new working medium, comprised of relatively high-mass nanoparticles that will be accelerated to very high kinetic energies. The best performing electric thrusters in the present are able to deliver up to 15.000s specific impulse, but the new thruster is expected to deliver between 18.000 and 30.000s optimal specific impulse. This extraordinary property will increase with the equal amount of deliverable ideal velocity during an interplanetary mission.

  • Staging Mechanism Status of the Orbital Launcher NERVA

    61th International Astronautical Congress 8, IAC-10.D2.7.6

    The NERVA small orbital launcher under development is based on the adoption of the three parallel and planar boosters for the first stage. The booster solid propellant rocket engines are derived from the originating SA-2 missile design, otherwise largely transformed. Due to the very high thrust enhancement achieved by the first stage, which ends in unusually high levels of loading during the lift-off of more than 40 g-s, this conceptual solution proves quite challenging. There is no connection…

    The NERVA small orbital launcher under development is based on the adoption of the three parallel and planar boosters for the first stage. The booster solid propellant rocket engines are derived from the originating SA-2 missile design, otherwise largely transformed. Due to the very high thrust enhancement achieved by the first stage, which ends in unusually high levels of loading during the lift-off of more than 40 g-s, this conceptual solution proves quite challenging. There is no connection between the NERVA-Near Earth Exit and Reentry Vehicle Assessor and the old, nuclear bomb propulsion system with the same acronym.

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  • English

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  • German

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  • Hungarian

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  • Romanian

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  • Dutch

    Elementary proficiency

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