Patents by Inventor Jon V. Osborn

Jon V. Osborn 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: 8904887
    Abstract: A radio-frequency transparent window having internal conduits for the passage of cooling fluid is configured for simulating a highly uniform thermal environment for testing a device intended for use in space. The device to be tested is placed within a chamber in which a vacuum condition is maintained by a radio-frequency transparent pressure window under a pressure seal. Within the chamber, the thermal window is positioned adjacent, but not in contact with, the pressure window. A radio frequency signal is capable of passing directly through both the thermal window and the pressure window to permit communication with the device being tested within the housing. The thermal window is not in contact with the device so there in no conduction of heat from the device. Radiant heat transfer may occur from the device to the thermal window.
    Type: Grant
    Filed: November 17, 2011
    Date of Patent: December 9, 2014
    Assignee: The Aerospace Corporation
    Inventors: Michael A. Tockstein, James P. Nokes, Jon V. Osborn, Dhruv N. Patel, Alan R. Hopkins, John S. Williams, Gary N. Harper
  • Publication number: 20130125676
    Abstract: A radio-frequency transparent window having internal conduits for the passage of cooling fluid is configured for simulating a highly uniform thermal environment for testing a device intended for use in space. The device to be tested is placed within a chamber in which a vacuum condition is maintained by a radio-frequency transparent pressure window under a pressure seal. Within the chamber, the thermal window is positioned adjacent, but not in contact with, the pressure window. A radio frequency signal is capable of passing directly through both the thermal window and the pressure window to permit communication with the device being tested within the housing. The thermal window is not in contact with the device so there in no conduction of heat from the device. Radiant heat transfer may occur from the device to the thermal window.
    Type: Application
    Filed: November 17, 2011
    Publication date: May 23, 2013
    Applicant: THE AEROSPACE CORPORATION
    Inventors: MICHAEL A. TOCKSTEIN, JAMES P. NOKES, JON V. OSBORN, DHRUV N. PATEL, ALAN R. HOPKINS, JOHN S. WILLIAMS
  • Patent number: 8325776
    Abstract: A device having a light cavity includes, at one end, a plasmonic reflector having a grating surface for coupling incoming light into traverse plasmon waves and for coupling the traverse plasmon wave into broaden light, the surface serving to redistribute light within the cavity, the reflector being well suited for use in laser diodes for redistributing filamental cavity laser light into spatially broaden cavity laser light for translating multimodal laser light into unimodal laser light for improved reliability and uniform laser beam creation.
    Type: Grant
    Filed: July 22, 2011
    Date of Patent: December 4, 2012
    Assignee: The Aerospace Corporation
    Inventors: Joshua A. Conway, Jon V. Osborn, Ryan A. Stevenson
  • Publication number: 20110280273
    Abstract: A device having a light cavity includes, at one end, a plasmonic reflector having a grating surface for coupling incoming light into traverse plasmon waves and for coupling the traverse plasmon wave into broaden light, the surface serving to redistribute light within the cavity, the reflector being well suited for use in laser diodes for redistributing filamental cavity laser light into spatially broaden cavity laser light for translating multimodal laser light into unimodal laser light for improved reliability and uniform laser beam creation.
    Type: Application
    Filed: July 22, 2011
    Publication date: November 17, 2011
    Inventors: Joshua A. Conway, Jon V. Osborn, Ryan A. Stevenson
  • Patent number: 8009716
    Abstract: A device having a light cavity includes, at one end, a plasmonic reflector having a grating surface for coupling incoming light into traverse plasmon waves and for coupling the traverse plasmon wave into broaden light, the surface serving to redistribute light within the cavity, the reflector being well suited for use in laser diodes for redistributing filamental cavity laser light into spatially broaden cavity laser light for translating multimodal laser light into unimodal laser light for improved reliability and uniform laser beam creation.
    Type: Grant
    Filed: October 29, 2007
    Date of Patent: August 30, 2011
    Assignee: The Aerospace Corporation
    Inventors: Joshua A. Conway, Jon V. Osborn, Ryan A. Stevenson
  • Patent number: 7960753
    Abstract: A surface plasmon polaritron activated semiconductor device uses a surface plasmon wire that functions as an optical waveguide for fast communication of a signal and functions as a energy translator using a wire tip for translating the optical signal passing through the waveguide into plasmon-polaritron energy at a connection of the semiconductor device, such as a transistor, to activate the transistor for improved speed of communications and switching for preferred use in digital systems.
    Type: Grant
    Filed: September 11, 2007
    Date of Patent: June 14, 2011
    Assignee: The Aerospace Corporation
    Inventors: Joshua A. Conway, Ryan A. Stevenson, Jon V. Osborn
  • Patent number: 7719693
    Abstract: A stroboscopic imaging interferometer system includes an environmental chamber having a novel viewing window equipped with a rigidly integrated beam splitter and piezo actuated reference mirror for illuminating a device providing an object beam and reference mirror for providing a reference beam, upon the reflection of both beams, produces interference of the object beam by the reference beam for providing absolute phase observations of the device, that may be a MEMS device under test.
    Type: Grant
    Filed: April 23, 2007
    Date of Patent: May 18, 2010
    Assignee: The Aerospace Corporation
    Inventors: Jon V. Osborn, Josh A. Conway, Jesse D. Fowler
  • Publication number: 20090110021
    Abstract: A device having a light cavity includes, at one end, a plasmonic reflector having a grating surface for coupling incoming light into traverse plasmon waves and for coupling the traverse plasmon wave into broaden light, the surface serving to redistribute light within the cavity, the reflector being well suited for use in laser diodes for redistributing filamental cavity laser light into spatially broaden cavity laser light for translating multimodal laser light into unimodal laser light for improved reliability and uniform laser beam creation.
    Type: Application
    Filed: October 29, 2007
    Publication date: April 30, 2009
    Inventors: Joshua A. Conway, Jon V. Osborn, Ryan A. Stevenson
  • Publication number: 20090065801
    Abstract: A surface plasmon polaritron activated semiconductor device uses a surface plasmon wire that functions as an optical waveguide for fast communication of a signal and functions as a energy translator using a wire tip for translating the optical signal passing through the waveguide into plasmon-polaritron energy at a connection of the semiconductor device, such as a transistor, to activate the transistor for improved speed of communications and switching for preferred use in digital systems.
    Type: Application
    Filed: September 11, 2007
    Publication date: March 12, 2009
    Inventors: Joshua A. Conway, Ryan A. Stevenson, Jon V. Osborn
  • Publication number: 20080259344
    Abstract: A stroboscopic imaging interferometer system includes an environmental chamber having a novel viewing window equipped with a rigidly integrated beam splitter and piezo actuated reference mirror for illuminating a device providing an object beam and reference mirror for providing a reference beam, upon the reflection of both beams, produces interference of the object beam by the reference beam for providing absolute phase observations of the device, that may be a MEMS device under test.
    Type: Application
    Filed: April 23, 2007
    Publication date: October 23, 2008
    Inventors: Jon V. Osborn, Josh A. Conway, Jesse D. Fowler
  • Patent number: 7005713
    Abstract: An annular segment MOSFET structure has reduced drain electric fields for a given applied voltage and dimensional sizing for improved reliability from damage by reducing high energy hot carriers laterally traversing the channel by reducing the intensity of electric fields in the MOSFET structure by creating diverging electric field lines with decreased electric field strength at the drain, while enabling compact integrated layouts of multiple MOSFETs within a square area of surface silicon.
    Type: Grant
    Filed: December 1, 2003
    Date of Patent: February 28, 2006
    Assignee: The Aerospace Corporation
    Inventors: Donald C. Mayer, Jon V. Osborn, Ronald C. Lacoe, Everett E. King
  • Patent number: 6861633
    Abstract: An integrated microelectromechanical system (MEMS) sun sensor includes a filter, microlens, aperture and a folded MEMS optical element combined with an active pixel sensor array to form an integrated spacecraft sun sensor in an integrated sealed package, offering lower power, smaller size and higher performance for use on spinning spacecraft useful in attitude determinations. Multiple like sun sensors can be disposed for increasing the reliability, spatial coverage or spatial resolution for a specific performance requirement.
    Type: Grant
    Filed: June 20, 2002
    Date of Patent: March 1, 2005
    Assignee: The Aerospace Corporation
    Inventor: Jon V. Osborn
  • Publication number: 20030234341
    Abstract: An integrated microelectromechanical system (MEMS) sun sensor includes a filter, microlens, aperture and a folded MEMS optical element combined with an active pixel sensor array to form an integrated spacecraft sun sensor in an integrated sealed package, offering lower power, smaller size and higher performance for use on spinning spacecraft useful in attitude determinations. Multiple like sun sensors can be disposed for increasing the reliability, spatial coverage or spatial resolution for a specific performance requirement.
    Type: Application
    Filed: June 20, 2002
    Publication date: December 25, 2003
    Inventor: Jon V. Osborn
  • Patent number: 6483368
    Abstract: An address element, including a polysilicon resistor functioning as a heating element and blocking diode preventing sneak current to unaddressed elements, is selectively addressed using row and column address lines in a thin film structure having a minimum number of address lines and a minimum number of layers. The resistor heater element is well suited for igniting a fuel cell such as a fuel cell in an array of fuel cells disposed in a thin film microthruster.
    Type: Grant
    Filed: February 20, 2002
    Date of Patent: November 19, 2002
    Assignee: The Aerospace Corporation
    Inventors: Donald C. Mayer, Jon V. Osborn, Siegfried W. Janson, Peter D. Fuqua
  • Patent number: 6437640
    Abstract: An address element, including a polysilicon resistor functioning as a heating element and blocking diode preventing sneak current to unaddressed elements, is selectively addressed using row and column address lines in a thin film structure having a minimum number of address lines and a minimum number of layers. The resistor heater element is well suited for igniting a fuel cell such as a fuel cell in an array of fuel cells disposed in a thin film microthruster.
    Type: Grant
    Filed: September 12, 2000
    Date of Patent: August 20, 2002
    Assignee: The Aerospace Corporation
    Inventors: Donald C. Mayer, Jon V. Osborn, Siegfried W. Janson, Peter D. Fuqua
  • Publication number: 20020097079
    Abstract: An address element, including a polysilicon resistor functioning as a heating element and blocking diode preventing sneak current to unaddressed elements, is selectively addressed using row and column address lines in a thin film structure having a minimum number of address lines and a minimum number of layers. The resistor heater element is well suited for igniting a fuel cell such as a fuel cell in an array of fuel cells disposed in a thin film microthruster.
    Type: Application
    Filed: February 20, 2002
    Publication date: July 25, 2002
    Applicant: The Aerospace Corporation
    Inventors: Donald C. Mayer, Jon V. Osborn, Siegfried W. Janson, Peter D. Fuqua
  • Patent number: 6403403
    Abstract: The method addresses and interrogates addressable cells having at least one element including a polysilicon resistor functioning as a heating element and blocking diode preventing sneak current to un addressed elements, for selectively addressing one of the cells using row and column address line in a thin film structure having a minimum number of address lines and a minimum number of layers. The resistor heating element can be used for igniting a respective fuel cell in an array of fuel cells disposed in a thin film microthruster. After ignition, the address lines are used to interrogate the cell location for verification of fuel cell ignition well suited for monitoring fuel burns and usage of the microthruster.
    Type: Grant
    Filed: September 12, 2000
    Date of Patent: June 11, 2002
    Assignee: The Aerospace Corporation
    Inventors: Donald C. Mayer, Jon V. Osborn, Siegfried W. Janson, Peter D. Fuqua
  • Patent number: 6284966
    Abstract: A power sphere preferably used as part of a nanosatellite is formed using a plurality of flat panels solar arrays interconnected together by rotating hinges to approximate a spherical shape for use as an enclosure of a payload. The solar array panels are supported by an extending internal strut. The spherical shape provides attitude insensitive solar energy collection and heat radiation.
    Type: Grant
    Filed: March 6, 2000
    Date of Patent: September 4, 2001
    Assignee: The Aerospace Corporation
    Inventors: Edward J. Simburger, David A. Hinkley, Ernest Y. Robinson, David G. Gilmore, Jon V. Osborn