Patents by Inventor Raymond Edward Fraze

Raymond Edward Fraze 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).

  • Patent number: 10689131
    Abstract: A satellite configuration includes a plurality of individual satellite buses each having a number of side panels that form a polygonal shape, where the individual satellite buses collectively fit together to form the satellite configuration having a regular polygon shape. A method of producing the satellite configuration includes forming a plurality of individual satellite buses each having a polygonal shape, and fitting the individual satellite buses together to form the satellite configuration in a regular polygonal shape.
    Type: Grant
    Filed: July 6, 2018
    Date of Patent: June 23, 2020
    Assignee: Lockheed Martin Corporation
    Inventor: Raymond Edward Fraze
  • Patent number: 10538341
    Abstract: A self-mating modular satellite bus includes a plurality of side panels each having a front surface flanked by a first longitudinal edge and a second longitudinal edge, wherein the first longitudinal edge of each side panel is nested with the second longitudinal edge of an adjacent side panel. The longitudinal edges, when superimposed, form a joggle. A method of producing the modular satellite bus includes forming a plurality of the panels, aligning the first longitudinal edge of each side panel with the second longitudinal edge of an adjacent side panel, such that the first longitudinal edge of each side panel is nested with the second longitudinal edge of the adjacent side panel, and securing the first longitudinal edge of each side panel to the second longitudinal edge of the adjacent side panel.
    Type: Grant
    Filed: July 6, 2018
    Date of Patent: January 21, 2020
    Assignee: Vector Launch Inc.
    Inventor: Raymond Edward Fraze
  • Publication number: 20200010221
    Abstract: A satellite configuration includes a plurality of individual satellite buses each having a number of side panels that form a polygonal shape, where the individual satellite buses collectively fit together to form the satellite configuration having a regular polygon shape. A method of producing the satellite configuration includes forming a plurality of individual satellite buses each having a polygonal shape, and fitting the individual satellite buses together to form the satellite configuration in a regular polygonal shape.
    Type: Application
    Filed: July 6, 2018
    Publication date: January 9, 2020
    Applicant: Vector Launch, Inc.
    Inventor: Raymond Edward Fraze
  • Publication number: 20200010220
    Abstract: A self-mating modular satellite bus includes a plurality of side panels each having a front surface flanked by a first longitudinal edge and a second longitudinal edge, wherein the first longitudinal edge of each side panel is nested with the second longitudinal edge of an adjacent side panel. The longitudinal edges, when superimposed, form a joggle. A method of producing the modular satellite bus includes forming a plurality of the panels, aligning the first longitudinal edge of each side panel with the second longitudinal edge of an adjacent side panel, such that the first longitudinal edge of each side panel is nested with the second longitudinal edge of the adjacent side panel, and securing the first longitudinal edge of each side panel to the second longitudinal edge of the adjacent side panel.
    Type: Application
    Filed: July 6, 2018
    Publication date: January 9, 2020
    Applicant: Vector Launch, Inc.
    Inventor: Raymond Edward Fraze
  • Patent number: 7753207
    Abstract: A light-weight capsule having internal components comprised of sample containers with living organisms in solid and liquid form, inner carrier, multiple seals is disclosed to protect the samples contained within and to withstand an impact of up to 4000 G in outer space or Earth applications being subject to extreme conditions of varying radiation, temperature, pressure, and shock. The present capsule provides a compact and durable design with features for reducing size, mass and weight while increasing strength, structural integrity, and sealing strength to protect the samples contained interiorly and to withstand extreme conditions for travel in deep space or inhospitable places on Earth.
    Type: Grant
    Filed: April 6, 2008
    Date of Patent: July 13, 2010
    Assignee: The Planetary Society
    Inventors: Raymond Edward Fraze, Louis D. Friedman
  • Publication number: 20090250556
    Abstract: A light-weight capsule having internal components comprised of sample containers with living organisms in solid and liquid form, inner carrier, multiple seals is disclosed to protect the samples contained within and to withstand an impact of up to 4000 G in outer space or Earth applications being subject to extreme conditions of varying radiation, temperature, pressure, and shock. The present capsule provides a compact and durable design with features for reducing size, mass and weight while increasing strength, structural integrity, and sealing strength to protect the samples contained interiorly and to withstand extreme conditions for travel in deep space or inhospitable places on Earth.
    Type: Application
    Filed: April 6, 2008
    Publication date: October 8, 2009
    Applicant: THE PLANETARY SOCIETY
    Inventors: Raymond Edward Fraze, Louis D. Friedman