Patents Assigned to Northrop Grumman Space & Missions
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Patent number: 7980514Abstract: One embodiment of the invention includes a spacecraft. The spacecraft comprises at least one solar array panel comprising an array of solar cell sections. Each of the solar cell sections can be configured to generate electrical power from received solar radiation. The spacecraft also comprises a solar array selection controller configured to selectively deactivate a portion of the array of solar cell sections to generate a torque on the spacecraft based on a difference in at least one of solar and thermal radiation pressure between an activated portion of the array of solar cell sections and the deactivated portion of the array of solar cell sections.Type: GrantFiled: March 14, 2008Date of Patent: July 19, 2011Assignee: Northrop Grumman Space & Mission Systems Corp.Inventors: James Wehner, Lael Rudd, Christian Harris, Shahram Foroozan
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Patent number: 7965183Abstract: One embodiment of the present invention includes a system for determining authenticity of substances. The system comprises a plurality of RF sensors distributed in a predefined location pattern relative to a location for placing a substance under analysis. Each of the RF sensors is configured to transmit a response to an interrogation signal with a unique identifier. The system also comprises an RF transmitter that transmits sequences of interrogation signals over different frequency bands at one or more power levels and an RF receiver that receives responses to the sequences of interrogation signals transmitted from the RF sensors. The system further comprises a response pattern analyzer that determines response patterns for the RF sensors to the interrogation sequences and transmits a difference indicator if at least one of the determined response patterns varies from as predetermined signature of an authentic substance.Type: GrantFiled: July 10, 2007Date of Patent: June 21, 2011Assignee: Northrop Grumman Space and Mission Systems CorporationInventor: Vibeke Libby
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Patent number: 7956806Abstract: Systems and methods are provided for orienting an antenna in a communications system on a mobile platform to orient a peak of the antenna pattern in a direction associated with a signal source. A signal from a signal source is received at the antenna. A signal strength is measured from the received signal. A signal strength and a misalignment of the antenna along at least one axis are predicted according to a previous estimate of the signal strength, a previous estimate of the misalignment of the antenna, an estimated change in the signal strength, and a known change in the antenna orientation. The predicted signal strength and misalignment of the antenna are updated according to the measured signal strength to provide an estimate of a current misalignment of the antenna. The orientation of the peak of the antenna pattern is adjusted according to the estimated current misalignment of the antenna.Type: GrantFiled: June 15, 2009Date of Patent: June 7, 2011Assignee: Northrop Grumman Space and Mission Systems Corp.Inventors: Zhang Liu, Gregory A. Shreve
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Patent number: 7957439Abstract: A laser diode package includes a laser diode, a cooler, and a metallization layer. The laser diode is used for converting electrical energy to optical energy. The cooler receives and routes a coolant from a cooling source via internal channels. The cooler includes a plurality of ceramic sheets and a highly thermally-conductive sheet. The ceramic sheets are fused together and the thermally-conductive sheet is attached to a top ceramic sheet of the plurality of ceramic sheets. The metallization layer has at least a portion on the thermally-conductive sheet. The portion is electrically coupled to the laser diode for conducting the electrical energy to the laser diode.Type: GrantFiled: December 1, 2009Date of Patent: June 7, 2011Assignee: Northrop Grumman Space & MissionsInventors: Edward F. Stephens, Steven M. Coleman
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Patent number: 7939792Abstract: A light-powered data acquisition and control system immune to electromagnetic interference employs smart sensors in a network configuration capable of decentralized communication. A smart sensor with integral transducer encloses a microprocessor, fiber optic transceiver, and photovoltaic converter within a Faraday cage. Optical fibers link plural sensors for duplex communication with a fiber optic splitter, which transmits high intensity light to the converter for powering the sensors. The sensor converts analog input from the transducer into bit packets for fiber optic transmission to the network via the splitter. Firmware in the splitter converts the bit packets to network protocol and vice versa enabling data communication among sensors, splitters, and control receivers. Verification algorithms for testing sensors are run automatically by the microprocessor or through commands issued via the network. Mnemonics stored in the sensors provide automatic updating of system configuration.Type: GrantFiled: April 25, 2008Date of Patent: May 10, 2011Assignee: Northrop Grumman Space & Mission Systems Corp.Inventors: Johannes F. Nyffenegger, Robert E. Redmer
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Publication number: 20110032602Abstract: A fiber laser amplifier system including a master oscillator that generates a signal beam. A splitter splits the signal beam into a plurality of fiber beams where a separate fiber beam is sent to a fiber amplifier for amplifying the fiber beam. A tapered fiber bundle couples all of the output ends of all of the fiber amplifiers into a combined fiber providing a combined output beam. An end cap is optically coupled to an output end of the tapered fiber bundle to expand the output beam.Type: ApplicationFiled: August 7, 2009Publication date: February 10, 2011Applicant: Northrop Grumman Space & Mission Systems Corp.Inventor: Joshua Elliott Rothenberg
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Publication number: 20110032604Abstract: A fiber laser amplifier system including a beam splitter that splits a feedback beam into a plurality of fiber beams where a separate fiber beam is sent to a fiber amplifier for amplifying the fiber beam. A tapered fiber bundle couples all of the output ends of all of the fiber amplifiers into a combined fiber providing a combined output beam. An end cap is optically coupled to an output end of the tapered fiber bundle to expand the output beam. A beam sampler samples a portion of the output beam from the end cap and provides a sample beam. A single mode fiber receives the sample beam from the beam sampler and provides the feedback beam.Type: ApplicationFiled: August 7, 2009Publication date: February 10, 2011Applicant: Northrop Grumman Space & Mission Systems Corp.Inventors: Joshua Elliott Rothenberg, Eric Chiu Tat Cheung
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Publication number: 20100328760Abstract: A waveguide parametric device including a multi-mode waveguide having orientation layers formed in a propagation direction of a signal beam and a pump beam propagating down the waveguide. The orientation layers are oppositely oriented to provide non-linear coupling between the pump beam and the signal beam and have a periodicity that provides quasi-phase matching for a fundamental propagation mode, where the waveguide has a size to accommodate multi-mode wave propagation.Type: ApplicationFiled: August 14, 2008Publication date: December 30, 2010Applicant: Northrop Grumman Space & Mission Systems Corp.Inventors: Robert R. Rice, Elizabeth Twyford Kunkee, Peter Y.M. Livingston
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Patent number: 7852622Abstract: A vehicle has a personnel compartment including a necessary driving volume. A deployable display apparatus provides a plurality of visual display units to a vehicle. The vehicle has a personnel compartment including a necessary driving volume. At least one display housing is provided. Each display housing is configured to support at least one visual display unit. The visual display unit is configured to selectively provide visual information to an operator. At least one mounting arm has spaced-apart first and second arm ends. The first arm end is stationary relative to a base surface. The second arm end is attached to the display housing. The mounting arm is configured to selectively move the display housing between stowed and deployed positions such that at least one display housing, when in the deployed position, at least partially occupies the necessary driving volume, and the display housing, when in the stowed position, is wholly outside the necessary driving volume.Type: GrantFiled: December 20, 2007Date of Patent: December 14, 2010Assignee: Northrop Grumman Space & Mission Systems CorporationInventors: Bran Ferren, Dana Klaren, Lars Jangaard, Christian Carlberg, Clinton Blake Hope
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Patent number: 7812758Abstract: One embodiment of the invention includes a synthetic aperture radar (SAR) system. The system comprises a radar transmitter configured to transmit a combined signal, the combined signal comprising a first signal that is a modulated SAR radar signal and a second signal that is a modulated signal. The system also comprises at least one radar receiver configured to receive a reflected combined signal that comprises a reflected first signal and a reflected second signal, and to demodulate the reflected first and second signals. The reflected first and second signals can correspond to the first and second signals having been reflected from a target. The system further comprises a radar image processor configured to generate a radar image of the target based on signal parameters associated with the reflected first signal and based on information comprised within the reflected second signal.Type: GrantFiled: November 27, 2007Date of Patent: October 12, 2010Assignee: Northrop Grumman Space and Mission Systems CorporationInventor: James Richard Morris
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Patent number: 7800766Abstract: A method and apparatus 10 for detecting the height of non-flat and transparent substrates using one or more reflectors 30 patterned on the surface of the substrate 40 and adjusting the position of the substrate in its holder based on measurement of the height of the reflectors in comparison to a calibration marker 60 on the holder and using appropriate spacers 50 with appropriate thickness to adjust the placement of the substrate at various locations to place the greatest portion of the substrate in an optimal focal range of the lithography system.Type: GrantFiled: September 21, 2007Date of Patent: September 21, 2010Assignee: Northrop Grumman Space & Mission Systems Corp.Inventors: Carol Osaka Namba, Po-Hsin Liu, Ioulia Smorchkova, Mike Wojtowicz, Rob Coffie
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Patent number: 7773307Abstract: Systems and methods for shifting the phase of incident light to induce a continuous phase variation in an azimuthal direction. A phase mask assembly has a first surface and a second surface. The first surface and the second surface are configured such that the distance between the first surface and the second surface varies continuously in an azimuthal direction around the phase mask. This mask can be used in a coronagraph system to effectively suppress the on-axis star image for the detection of off-axis planets.Type: GrantFiled: December 12, 2006Date of Patent: August 10, 2010Assignee: Northrop Grumman Space & Mission Systems CorporationInventor: Chun-Ching Shih
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Publication number: 20100184262Abstract: A semiconductor device is fabricated to include source and drain contacts including an ohmic metal sunken into the barrier layer and a portion of the channel layer; a protective dielectric layer disposed between the source and drain contacts on the barrier layer; a metallization layer disposed in drain and source ohmic vias between the source contact and the protective dielectric layer and between the protective dielectric layer and the drain contact; and a metal T-gate disposed above the barrier layer including a field mitigating plate disposed on a side portion of a stem of the metal T-gate.Type: ApplicationFiled: March 25, 2010Publication date: July 22, 2010Applicant: Northrop Grumman Space and Mission Systems Corp.Inventors: Ioulia Smorchkova, Robert Coffie, Ben Heying, Carol Namba, Po-Hsin Liu, Boris Hikin
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Patent number: 7751779Abstract: A payload (108) to be mounted onto a satellite (102) can include a first steerable antenna (302) providing a downlink to and an uplink from a first user terminal; a second steerable antenna (304) providing a downlink to and an uplink from a second user terminal; a switching network (306) coupling the first steerable antenna to the second steerable antenna; and a payload control unit (120) controlling the switching network to select one of the downlink to the first user terminal provided by the first steerable antenna and the downlink to the second user terminal provided by the second steerable antenna, and one of the uplink from the first user terminal provided by the first steerable antenna and the uplink from the second user terminal provided by the second steerable antenna.Type: GrantFiled: December 21, 2006Date of Patent: July 6, 2010Assignee: Northrop Grumman Space & Mission Systems Corp.Inventors: Hau H. Ho, Ethan A. Stein, Michael Fashano, Peter J. Hadinger, Gary Lehto
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Patent number: 7750370Abstract: A semiconductor device is fabricated to include source and drain contacts including an ohmic metal sunken into the barrier layer and a portion of the channel layer; a protective dielectric layer disposed between the source and drain contacts on the barrier layer; a metallization layer disposed in drain and source ohmic vias between the source contact and the protective dielectric layer and between the protective dielectric layer and the drain contact; and a metal T-gate disposed above the barrier layer including a field mitigating plate disposed on a side portion of a stem of the metal T-gate.Type: GrantFiled: December 20, 2007Date of Patent: July 6, 2010Assignee: Northrop Grumman Space & Mission Systems Corp.Inventors: Ioulia Smorchkova, Robert Coffie, Ben Heying, Carol Namba, Po-Hsin Liu, Boris Hikin
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Patent number: 7745777Abstract: In accordance with yet another aspect of the present invention, an active imaging system is provided for imaging a target of interest. An imaging assembly includes a light source and an optical assembly comprising a plurality of passive optical components. The optical assembly divides received light into a first beam, having a first polarization and a second beam, having a second, orthogonal polarization, directs the first and second beam along respective first and second optical paths within the optical assembly, and recombines the first and second beams into a combined beam. A sensor detects the combined beam.Type: GrantFiled: March 11, 2008Date of Patent: June 29, 2010Assignee: Northrop Grumman Space and Mission Systems Corp.Inventor: Bo Su Chen
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Patent number: 7733194Abstract: A modulator is provided that comprises a nonlinear transmission line (NLTL) that is bias modulated by a baseband signal. A given logic state of the baseband signal determines a delay amount of a first carrier signal through the NLTL. The modulator further comprises an impulse forming network (IFN) that includes a first NLTL that receives the first carrier signal delayed by the determined delay amount and a second NLTL that receives a second carrier signal having a fixed delay amount. The first NLTL and second NLTL within the IFN have opposite diode polarity configurations. The modulator further comprises a power combiner that converts a delta delay of the first carrier signal relative to the second carrier signal to a sharp impulse that represents the given logic state of the baseband signal.Type: GrantFiled: November 2, 2007Date of Patent: June 8, 2010Assignee: Northrop Grumman Space and Mission Systems CorporationInventors: Xing Lan, Mark Kintis, Flavia S. Fong
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Publication number: 20100127240Abstract: A device and method associated with carbon nanowires, such as single walled carbon nanowires having a high degree of alignment are set forth herein. A catalyst layer is deposited having a predetermined crystallographic configuration so as to control a growth parameter, such as an alignment direction, a diameter, a crystallinity and the like of the carbon nanowire. The catalyst layer is etched to expose a sidewall portion. The carbon nanowire is nucleated from the exposed sidewall portion. An electrical circuit device can include a single crystal substrate, such as Silicon, and a crystallographically oriented catalyst layer on the substrate having an exposed sidewall portion. In the device, carbon nanowires are disposed on the single crystal substrate aligned in a direction associated with the crystallographic properties of the catalyst layer.Type: ApplicationFiled: January 21, 2010Publication date: May 27, 2010Applicant: NORTHROP GRUMMAN SPACE & MISSION SYSTEMS CORP.Inventors: Vincent Gambin, Roger Su-Tsung Tsai
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Patent number: 7715099Abstract: Systems and methods for attenuating light from undesired sources in a coronagraph apparatus are provided. The coronagraph includes a first imaging lens that receives light representing a desired image and an undesired central image and a reimaging system that mitigates the undesired central image. The reimaging system includes a composite half-wave plate assembly that includes a plurality of angular half-wave plate sections. Each of the plurality of angular half-wave plate sections have two congruent sides that meet at an apex substantially at a center of the composite half-wave plate. A characteristic c-axis associated with a given angular half-wave plate section is aligned differently from the respective characteristic c-axes of at least two angular half-wave plate sections in substantial contact with the two sides of the given angular half-wave plate section. A fixation element engages the half-wave plate sections to maintain the angular half-wave plate sections in a desired arrangement.Type: GrantFiled: December 12, 2006Date of Patent: May 11, 2010Assignee: Northrop Grumman Space & Mission Systems CorporationInventor: Chun-Ching Shih
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Patent number: 7710639Abstract: A system and method is provided for uniform illumination of a target area. In one embodiment, the system comprises a plurality of mutually incoherent light sources configured to generate respective light beams with different wavelengths, and transmitting optics configured to transmit the light beams with different wavelengths in a non-overlapping wavelength light beam pattern over the target area, such that there are no overlap regions of the target area illuminated by a light beam from the same light source.Type: GrantFiled: December 12, 2006Date of Patent: May 4, 2010Assignee: Northrop Grumman Space & Mission Systems CorporationInventors: William Bryan Cottingame, Robert Rex Rice, Martin Richard Flannery