Patents by Inventor John Francis Dargin, III

John Francis Dargin, III has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Removing orbital space debris from near earth orbit
    Patent number: 11420776
    Abstract: A system utilizing an antenna generating an electromagnetic (EM) wave to interact with a solar EM wave to streamline magnetic flux in the polar cusp and to facilitate the flow of solar plasma through the Polar Cusp, resulting in an elevated plasma flux at the exit of the Polar Cusp. The elevated plasma flux intercepts and removes small space debris from Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO) and Geosynchronous Transfer Orbits (GTO) transiting the LEO altitude regimes.
    Type: Grant
    Filed: November 1, 2021
    Date of Patent: August 23, 2022
    Inventor: John Francis Dargin, III
  • Removing Orbital Space Debris from Near Earth Orbit
    Publication number: 20220073219
    Abstract: A system utilizing an antenna generating an electromagnetic (EM) wave to interact with a solar EM wave to streamline magnetic flux in the polar cusp and to facilitate the flow of solar plasma through the Polar Cusp, resulting in an elevated plasma flux at the exit of the Polar Cusp. The elevated plasma flux intercepts and removes small space debris from Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO) and Geosynchronous Transfer Orbits (GTO) transiting the LEO altitude regimes.
    Type: Application
    Filed: November 1, 2021
    Publication date: March 10, 2022
    Inventor: John Francis Dargin, III
  • Removing orbital space debris from near earth orbit
    Patent number: 11161632
    Abstract: A system utilizing an antenna generating an electromagnetic (EM) wave to interact with a solar EM wave to streamline magnetic flux in the polar cusp and to facilitate the flow of solar plasma through the Polar Cusp, resulting in an elevated plasma flux at the exit of the Polar Cusp. The elevated plasma flux intercepts and removes small space debris from Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO) and Geosynchronous Transfer Orbits (GTO) transiting the LEO altitude regimes.
    Type: Grant
    Filed: December 9, 2019
    Date of Patent: November 2, 2021
    Inventor: John Francis Dargin, III
  • Removing Orbital Space Debris From Near Earth Orbit
    Publication number: 20200223566
    Abstract: A system utilizing an antenna generating an electromagnetic (EM) wave to interact with a solar EM wave to streamline magnetic flux in the polar cusp and to facilitate the flow of solar plasma through the Polar Cusp, resulting in an elevated plasma flux at the exit of the Polar Cusp. The elevated plasma flux intercepts and removes small space debris from Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO) and Geosynchronous Transfer Orbits (GTO) transiting the LEO altitude regimes.
    Type: Application
    Filed: December 9, 2019
    Publication date: July 16, 2020
    Inventor: John Francis Dargin, III
  • Removing orbital space debris from near earth orbit
    Patent number: 10501212
    Abstract: A system utilizing an antenna generating an electromagnetic (EM) wave to interact with a solar EM wave to streamline magnetic flux in the polar cusp and to facilitate the flow of solar plasma through the Polar Cusp, resulting in an elevated plasma flux at the exit of the Polar Cusp. The elevated plasma flux intercepts and removes small space debris from Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO) and Geosynchronous Transfer Orbits (GTO) transiting the LEO altitude regimes.
    Type: Grant
    Filed: April 30, 2019
    Date of Patent: December 10, 2019
    Inventor: John Francis Dargin, III
  • Removing Orbital Space Debris From Near Earth Orbit
    Publication number: 20190329914
    Abstract: A system utilizing an antenna generating an electromagnetic (EM) wave to interact with a solar EM wave to streamline magnetic flux in the polar cusp and to facilitate the flow of solar plasma through the Polar Cusp, resulting in an elevated plasma flux at the exit of the Polar Cusp. The elevated plasma flux intercepts and removes small space debris from Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO) and Geosynchronous Transfer Orbits (GTO) transiting the LEO altitude regimes.
    Type: Application
    Filed: April 30, 2019
    Publication date: October 31, 2019
    Inventor: John Francis Dargin, III