The Aerospace Corporation

Jon Victor Osborn

Donald C Mayer

Ryan Allan Stevenson

Siegfried W Janson

Peter D Fuqua

Joshua A Conway

Edward J Simburger

James P Nokes

Dhruv N Patel

David A Hinkley

Jesse D Fowler

Ernest Y Robinson

Josh A Conway

David G Gilmore

John S Williams

Ronald C Lacoe

Everett E King

Gary N Harper

Michael A Tockstein

Alan R Hopkins

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.

Radio frequency transparent thermal window

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.

Plasmon stabilized laser diodes

Plasmon stabilized unimodal laser diodes

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.

Surface plasmon polariton actuated transistors

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.

Interferometry system chamber viewing window

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.

Annular segmented MOSFET

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.

Microelectromechanical system optical sensor providing bit image data of a viewed image

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.

Addressable diode isolated thin film cell array

Addressable diode isolated thin film array

A radio frequency (RF) microelectromechanical systems (MEMS) switch is manufactured by independent processing and subsequent bonding together of a MEMS substrate in alignment with an RF substrate. The RF MEMS switch is designed so as to encapsulate a flexing diaphragm supporting a switch electrode used with electrostatic flexing potentials to move electrodes of the MEMS substrate up and down over an RF transmission line structure of the RF substrate. The bonded combined MEMS switch structure is used to create an encapsulated RF MEMS switch suitable for direct coupling, AC coupling, and direct modulation of RF signals. The resulting MEMS RF switch device provides a reliable, minimally distorting RF transmission line geometry, free of contamination for use in high speed RF signal switching applications well suited for advance communication RF switching requirements.

RF MEMS switch

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.

Diode isolated thin film fuel cell array addressing method

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.

Growing community of inventors

Thousand Oaks, CA, United States of America

Jon Victor Osborn