Patents Assigned to Northrop Grumman Space & Mission Systems Corporation
  • Patent number: 7965183
    Abstract: 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: Grant
    Filed: July 10, 2007
    Date of Patent: June 21, 2011
    Assignee: Northrop Grumman Space and Mission Systems Corporation
    Inventor: Vibeke Libby
  • Patent number: 7852622
    Abstract: 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: Grant
    Filed: December 20, 2007
    Date of Patent: December 14, 2010
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Bran Ferren, Dana Klaren, Lars Jangaard, Christian Carlberg, Clinton Blake Hope
  • Patent number: 7812758
    Abstract: 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: Grant
    Filed: November 27, 2007
    Date of Patent: October 12, 2010
    Assignee: Northrop Grumman Space and Mission Systems Corporation
    Inventor: James Richard Morris
  • Patent number: 7773307
    Abstract: 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: Grant
    Filed: December 12, 2006
    Date of Patent: August 10, 2010
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventor: Chun-Ching Shih
  • Patent number: 7733194
    Abstract: 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: Grant
    Filed: November 2, 2007
    Date of Patent: June 8, 2010
    Assignee: Northrop Grumman Space and Mission Systems Corporation
    Inventors: Xing Lan, Mark Kintis, Flavia S. Fong
  • Patent number: 7715099
    Abstract: 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: Grant
    Filed: December 12, 2006
    Date of Patent: May 11, 2010
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventor: Chun-Ching Shih
  • Patent number: 7710639
    Abstract: 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: Grant
    Filed: December 12, 2006
    Date of Patent: May 4, 2010
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventors: William Bryan Cottingame, Robert Rex Rice, Martin Richard Flannery
  • Publication number: 20100029063
    Abstract: 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: Application
    Filed: January 16, 2007
    Publication date: February 4, 2010
    Applicant: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Vincent Gambin, Roger Su-Tsung Tsai
  • Patent number: 7656253
    Abstract: An apparatus in one example comprises a piezoelectric layer, an input transducer, an output transducer, and at least one electrode set. The input transducer is configured to convert an input signal from an input source to a surface acoustic wave and send the surface acoustic wave from an input portion of the piezoelectric layer to an output portion of the piezoelectric layer. The input transducer comprises a set of input passbands. The output transducer is configured to receive the surface acoustic wave from the output portion of the piezoelectric layer. The output transducer comprises a set of output passbands. The at least one electrode set is configured to apply at least one voltage bias to at least one portion of the piezoelectric layer to create an electric field that controls an acoustic velocity of the surface acoustic wave through the at least one portion of the piezoelectric layer.
    Type: Grant
    Filed: April 18, 2007
    Date of Patent: February 2, 2010
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Robert Bruce Stokes, Alvin Ming-Wei Kong
  • Patent number: 7635921
    Abstract: Self-powered mobile electrical power hubs are provided. In one embodiment, a self-powered electrical power hub comprises an internal combustion engine driven generator that provides electrical power and at least one electrically powered transport driver configured to facilitate movement of the self-powered mobile electrical power hub. The self-powered mobile electrical power hub further comprises an accessible power hub that provides external access to electrical power, wherein a substantial portion of the electrical power from the internal combustion engine driven generator is provided to power the at least one electrically powered transport driver in a transport mode and a substantial portion of the electrical power from the internal combustion engine driven generator is available at the accessible power hub in an idle mode.
    Type: Grant
    Filed: April 6, 2007
    Date of Patent: December 22, 2009
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Neil G. Siegel, Chris Hassapis, W. Daniel Hillis, Dan Danknick
  • Patent number: 7434947
    Abstract: Systems and methods for shifting the phase of incident light to induce a continuous phase variation in an azimuthal direction. A phase mask apparatus includes a conical mirror assembly and a flexible annular reflector that substantially surrounds at least a portion of the conical mirror assembly. The flexible annular reflector is configured to receive reflected light from the conical mirror assembly. A plurality of driver assemblies are operative to deform the flexible annular reflector as to produce the desired phase response in light reflected from the annular reflector.
    Type: Grant
    Filed: December 12, 2006
    Date of Patent: October 14, 2008
    Assignee: Northrop Grumman Space & Mission Systems Corporation
    Inventor: Chun-Ching Shih
  • Patent number: 7330491
    Abstract: A laser diode package (10) according to the present invention is tolerant of short-circuit and open-circuit failures. The laser diode package (10) includes a laser diode bar (12), a forward-biased diode (14), a heat sink (18), and a lid (16) which may have fusible links (86). The laser diode bar (12) and the forward-biased diode (14) are electrically connected in parallel between the heat sink (18) and the lid (16). The emitting region of the laser diode bar (12) is aligned to emit radiation away from the forward-biased diode (14). Several packages can be stacked together to form a laser diode array (42). The forward-biased diode (14) allows current to pass through it when an open-circuit failure has occurred in the corresponding laser diode bar (12), thus preventing an open-circuit failure from completely disabling the array (42).
    Type: Grant
    Filed: April 20, 2004
    Date of Patent: February 12, 2008
    Assignee: Northrop Grumman Space & Missions Systems Corporation
    Inventors: Edward F. Stephens, IV, Joseph L. Levy, John S. Whiteley
  • Publication number: 20050181616
    Abstract: Accordingly, this invention relates to an dry etching process for semiconductor wafers. More particularly, the present invention discloses a dry etching process including a halogen etchant (24) and a nitrogen gas (28) that selectively etches a compound semiconductor material (18) faster than the front-side metal layers (16A)(16B). Further, the dry etching process produces a vertical wall profile on compound semiconductor material (18) in both X (38) and Y (40) crystalline directions without undercutting the top of a via-opening.
    Type: Application
    Filed: February 18, 2004
    Publication date: August 18, 2005
    Applicant: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Jennifer Wang, Huai-Min Sheng, Mike Barsky
  • Publication number: 20050181618
    Abstract: An improved etching process for creating dimensionally accurate sub-micron and micron via-openings is disclosed. Specifically, this invention discloses a via etching process for a polymer layer (24) deposited on a semiconductor substrate (28) comprising the steps of: placing the semiconductor substrate comprising a polymer layer (24) deposited on the semiconductor substrate, a hard-mask (30) deposited on the polymer layer (24) and a photoresist mask (32) deposited on the hard-mask (30). The invention further, discloses performing a hard-mask opening step (34) comprising releasing a first fluoride gas (36) into the chamber. Furthermore, performing a polymer etching step (40) comprising releasing a second fluoride gas (42) into the chamber is disclosed. The invention also includes a hard-mask removal and tapered via step (46) to increase process margin.
    Type: Application
    Filed: February 17, 2004
    Publication date: August 18, 2005
    Applicant: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Jennifer Wang, Mike Barsky
  • Publication number: 20050178740
    Abstract: A method of dry plasma etching a semiconductor structure (20), having at least one semiconductor material layer (21), on a semiconductor wafer (200), involving a dry plasma reaction gas mixture (30i) being chemically selected for, and having an etch rate corresponding to, each semiconductor material layer (21); dividing the semiconductor structure (20) into a masked portion (23a) and an unmasked portion (23b); and sequentially exposing the unmasked portion (23b) of the semiconductor structure (20) to the dry plasma reaction gas mixture (30i).
    Type: Application
    Filed: February 18, 2004
    Publication date: August 18, 2005
    Applicant: Northrop Grumman Space & Mission Systems Corporation
    Inventor: Jennifer Wang
  • Publication number: 20050099222
    Abstract: An electronically programmable multimode circuit is described. More particularly, the present invention is an electronically programmable multimode circuit that includes a first path and a second path wherein a mode and a signal directional flow direction is controlled through the selective biasing of the first path and the second path. A multimode circuit is produced that contains modes such as a phase shifter mode, an IQ modulation mode, an amplifier mode, a mixer mode, and a multiplier mode.
    Type: Application
    Filed: November 10, 2003
    Publication date: May 12, 2005
    Applicant: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Jeffrey Yang, Matt Nishimoto, Xing Lan, Michael Battung, Robert Wang, Yun-Ho Chung
  • Publication number: 20050026571
    Abstract: A common source, bi-directional microwave amplifier is described. More particularly, the present invention is a microwave, common source, bi-directional amplifier that includes a first amplification path and a second amplification path wherein the signal directional flow is controlled through the selective biasing of the first amplification path and the second amplification path. Each amplification path is designed to optimize desired performance. For signal flow through the first amplification path, the first amplification path is biased-on and the second path is biased-off. For signal flow through the second amplification path, the second amplification path is biased-on and the first path is biased-off.
    Type: Application
    Filed: August 1, 2003
    Publication date: February 3, 2005
    Applicant: Northrop Grumman Space & Mission Systems Corporation
    Inventors: Jeffrey Yang, Matt Nishimoto, Yun-Ho Chung, Michael Battung, Richard Lai
  • Patent number: 6781447
    Abstract: A demodulator demodulates a modulated signal waveform in a data communication system. A phase tracking loop tracks the phase of said modulated signal waveform and having an inner block decoder configured to decode a set of vector pairs of the modulated signal waveform at a decode rate to generate associated codewords and phase estimates. A group of data symbols consisting of the first data symbols of the modulated signal waveform are run backwards through the phase tracking loop. An outer block decoder receives the associated codewords generated by said inner block decoder and utilizes and corrects only codewords associated with symbols after and including the group of data symbols consisting of the first data symbols of the modulated signal waveform.
    Type: Grant
    Filed: December 4, 2001
    Date of Patent: August 24, 2004
    Assignee: Northrop Grumman Space & Mission Systems Corporation Space Technology
    Inventors: Stuart T. Linsky, Scott A. Cooper, Christopher W. Walker, Ali R. Golshan