Patents Assigned to Space
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Patent number: 6714521Abstract: Provided is a system and method for implementing a constellation of satellites in inclined elliptical orbits that provides simplified satellite tracking for ground stations on the earth. The satellite orbits form a pair of repeating ground tracks around the earth. In each ground track the satellites operate only in active arcs well above or below the equator, emulating many of the characteristics of geostationary satellites. The parameters of the satellite orbits are adjusted so that the end points of the active arcs in the two ground tracks coincide; the turn-off point of an active arc in one ground track being the same as the turn-on point of an active arc in the other. For a ground station served by the satellites in these arcs, the active satellites appear to be moving slowly in one direction around a closed, teardrop-shaped path in the sky, at a generally high elevation angle.Type: GrantFiled: December 29, 2000Date of Patent: March 30, 2004Assignee: Space Resources International Ltd.Inventor: John E. Draim
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Patent number: 6710800Abstract: A displaying system capable of Internet communication and a control method thereof.Type: GrantFiled: April 16, 1999Date of Patent: March 23, 2004Assignee: Time & Space Tech. Co., Ltd.Inventor: Ki-Seok Park
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Patent number: 6710880Abstract: A high-precision heterodyne interferometer measures relative displacement by creating a thermally-insensitive system generally not subject to polarization leakage. By using first and second light beams separated by a small frequency difference (&Dgr;f), beams of light at the first frequency (f0) are reflected by co-axial mirrors, the first mirror of which has a central aperture through which the light is transmitted to and reflected by the second mirror. Prior to detection, the light beams from the two mirrors are combined with light of the second and slightly different frequency. The combined light beams are separated according to the light from the mirrors. The change in phase (&Dgr;&phgr;) with respect to the two signals is proportional to the change in distance of Fiducial B by a factor of wavelength (&lgr;) divided by 4&pgr; (&Dgr;L=&lgr;&Dgr;&phgr;1/(4&pgr;)). In a second embodiment, a polarizing beam splitting system can be used.Type: GrantFiled: September 6, 2001Date of Patent: March 23, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Feng Zhao
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Patent number: 6710352Abstract: A charged particle measuring apparatus discriminates the types of charged particles accurately and the energy precisely, measures high-energy charged particles precisely, and detects a failure of the apparatus to continue measurement in a mode corresponding to the failure. Outputs from first and second detectors are used as first and second addresses, respectively. The second detector includes a plurality of detectors. The output from a third detector is used as information about whether or not certain charged particles penetrate the second detector. The loss energy characteristics of charged particles to be measured are expressed in the first and second addresses. The number of times the charged particles are measured for loss energy are counted with respect to the addresses. When the series of detectors constituting the first, second, and third detectors suffers a failure, a measurement mode excluding any failed detector is employed to continue measurement.Type: GrantFiled: December 27, 2002Date of Patent: March 23, 2004Assignees: National Space Development Agency of Japan, Meisei Electric Co., Ltd.Inventors: Jun Kikuchi, Haruhisa Matsumoto, Hideki Koshiishi, Takashi Nozaki, Shigeru Takehisa
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Patent number: 6706549Abstract: A method of bulk manufacturing SiC sensors is disclosed and claimed. Materials other than SiC may be used as the substrate material. Sensors requiring that the SiC substrate be pierced are also disclosed and claimed. A process flow reversal is employed whereby the metallization is applied first before the recesses are etched into or through the wafer. Aluminum is deposited on the entire planar surface of the metallization. Photoresist is spun onto the substantially planar surface of the Aluminum which is subsequently masked (and developed and removed). Unwanted Aluminum is etched with aqueous TMAH and subsequently the metallization is dry etched. Photoresist is spun onto the still substantially planar surface of Aluminum and oxide and then masked (and developed and removed) leaving the unimidized photoresist behind. Next, ITO is applied over the still substantially planar surface of Aluminum, oxide and unimidized photoresist.Type: GrantFiled: April 12, 2002Date of Patent: March 16, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert S. Okojie
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Patent number: 6707429Abstract: The invention is embodied in a monolithic semiconductor integrated circuit in which is formed an antenna, such as a slot dipole antenna, connected across a rectifying diode. In the preferred embodiment, the antenna is tuned to received an electromagnetic wave of about 2500 GHz so that the device is on the order of a wavelength in size, or about 200 microns across and 30 microns thick. This size is ideal for mounting on a microdevice such as a microrobot for example. The antenna is endowed with high gain in the direction of the incident radiation by providing a quarter-wavelength (30 microns) thick resonant cavity below the antenna, the cavity being formed as part of the monolithic integrated circuit. Preferably, the integrated circuit consists of a thin gallium arsenide membrane overlying the resonant cavity and supporting an epitaxial Gallium Arsenide semiconductor layer.Type: GrantFiled: December 9, 2002Date of Patent: March 16, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Peter H. Siegel
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Patent number: 6702300Abstract: A high temperature sealing system is operative to seal an interface between adjacent hot structures and to minimize parasitic flow between such structures that move relative to one another in-plane or out-of-plane. The sealing system may be used to seal thrust-directing ramp structures of a reusable launch vehicle and includes a channel and a plurality of movable segmented sealing elements. Adjacent ramp structures include edge walls which extend within the channel. The sealing elements are positioned along the sides of the channel and are biased to engage with the inner surfaces of the ramp structures. The segmented sealing elements are movable to correspond to the contour of the thrust-directing ramp structures. The sealing system is operative to prevent high temperature thrust gases that flow along the ramp structures from infiltrating into the interior of the vehicle.Type: GrantFiled: January 11, 2002Date of Patent: March 9, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Bruce M. Steinetz, Patrick H. Dunlap, Jr.
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Patent number: 6703620Abstract: This invention has the ability to create Fourier-based images with only two grid pairs. The two grid pairs are manipulated in a manner that allows (1) a first grid pair to provide multiple real components of the Fourier-based image and (2) a second grid pair to provide multiple imaginary components of the Fourier-based image. The novelty of this invention resides in the use of only two grid pairs to provide the same imaging information that has been traditionally collected with multiple grid pairs.Type: GrantFiled: December 30, 1998Date of Patent: March 9, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Jonathan W. Campbell
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Patent number: 6704375Abstract: The device for the homodyne reception of optical phase-keyed signals comprises a heterodyne receiver (101, 102), a data discriminator (20), a frequency acquisition circuit (80) and a local oscillator laser (70). In addition, the device has a window discriminator circuit consisting of a window comparator (30) and a feedback unit (40), whose output is connected with the input of a reversing switch (50). The window comparator (30) has been inserted between the output of the heterodyne receiver (101, 102) and the one input of the feedback unit (40), whose other input is supplied with the output signal (Si) of the discriminator (20). The output of the frequency acquisition circuit (80) is connected with the other connector of the reversing switch (50), whose output signals supplied to the control input of the local oscillator laser (70). The window comparator (30) has two or more thresholds. The feedback unit (40) can have a control input for a quadrature channel (Sq).Type: GrantFiled: July 28, 1999Date of Patent: March 9, 2004Assignee: Contraves Space AGInventor: Christoph Peter Serbe
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Publication number: 20040040132Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises making a piezoelectric fiber sheet by providing a plurality of wafers of piezoelectric material, bonding the wafers together with an adhesive material to form a stack of alternating layers of piezoelectric material and adhesive material, and cutting through the stack in a direction substantially parallel to the thickness of the stack and across the alternating layers of piezoelectric material and adhesive material to provide at least one piezoelectric fiber sheet having two sides comprising a plurality of piezoelectric fibers in juxtaposition to the adhesive material. The method further comprises bonding two electrically conductive films to the two sides of the piezoelectric fiber sheet. At least one conductive film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezoelectric fiber sheet.Type: ApplicationFiled: September 3, 2003Publication date: March 4, 2004Applicant: USA as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: W. Keats Wilkie, Robert G. Bryant, Robert L. Fox, Richard F. Hellbaum, James W. High, Antony Jalink, Bruce D. Little, Paul H. Mirick
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Patent number: 6701126Abstract: Provided is an improved system and method for implementing a constellation of satellites in inclined elliptical orbits. The satellites are operated during the portion of their orbits near apogee to emulate the characteristics of geostationary satellites. The orbits are configured to form a number of closely spaced repeating ground tracks around the earth. In each ground track the satellites operate only in arcs well above or below the equator to provide a large number of non-geostationary orbital slots that substantially increase global satellite capacity without interfering with the existing geostationary satellite ring. Minimum spacing is maintained between satellites in each active arc and between satellites in the active arcs of adjacent ground tracks to ensure that the satellites in the non-geostationary constellation do not interfere with each other.Type: GrantFiled: November 13, 2000Date of Patent: March 2, 2004Assignee: Space Resource International Ltd.Inventor: John E. Draim
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Patent number: 6700298Abstract: A power source converts &agr;-particle energy to electricity for use in electrical systems. Liquid gallium or other liquid medium is subjected to &agr;-particle emissions. Electrons are freed by collision from neutral gallium atoms to provide gallium ions. The electrons migrate to a cathode while the gallium ions migrate to an anode. A current and/or voltage difference then arises between the cathode and anode because of the work function difference of the cathode and anode. Gallium atoms are regenerated by the receiving of electrons from the anode enabling the generation of additional electrons from additional &agr;-particle collisions.Type: GrantFiled: June 27, 2002Date of Patent: March 2, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: G. Jeffrey Snyder, Jagdishbhai Patel, Jean-Pierre Fleurial
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Patent number: 6701021Abstract: The present method relates to a method for encoding image data using vector quantization. According to the invention, a small first codebook is determined. Each image vector of the image data is then encoded by determining a codevector within the first codebook that best approximates the image vector within the image data. A first index map is generated by replacing each image vector with an index indicative of the codevector's location within the first codebook. Then difference data are evaluated based on the original image data and the encoded image data. Each error vector of the difference data is then encoded using another small codebook. In another index map the error vectors are then replaced with an index indicative of the codevector's location within the other codebook. Evaluation of the error based on the difference data and the encoded difference data provides new difference data which is used to evaluate the fidelity of the approximation process performed for compression.Type: GrantFiled: November 22, 2000Date of Patent: March 2, 2004Assignee: Canadian Space AgencyInventors: Shen-En Qian, Allan B. Hollinger
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Patent number: 6700656Abstract: An optical system, consisting of drop-reflection image, reflection-refracted shadowgraphy and top-view photography, is used to measure the spreading and instant dynamic contact angle of a volatile-liquid drop on a non-transparent substrate. The drop-reflection image and the shadowgraphy is shown by projecting the images of a collimated laser beam partially reflected by the drop and partially passing through the drop onto a screen while the top view photograph is separately viewed by use of a camera video recorder and monitor. For a transparent liquid on a reflective solid surface, thermocapillary convection in the drop, induced by evaporation, can be viewed nonintrusively, and the drop real-time profile data are synchronously recorded by video recording systems. Experimental results obtained from this technique clearly reveal that evaporation and thermocapillary convection greatly affect the spreading process and the characteristics of dynamic contact angle of the drop.Type: GrantFiled: September 17, 2002Date of Patent: March 2, 2004Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: David F. Chao, Nengli Zhang
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Patent number: 6699669Abstract: The present invention relates to improved techniques for separating cells, particles and molecules important to medical science and biotechnology because separation is frequently the limiting factor for many biological processes. The apparatus and method of use provides an innovative method for quantitatively separating cells, proteins, or other particles, using multistage, magnetically, electromagnetically assisted separation technology, (“MAGSEP”). The MAGSEP technology provides a separation technology applicable to medical, chemical, cell biology, and biotechnology processes. Moreover, the instant invention relates to a method for separating and isolating mixtures of combinatorial synthesized molecules such that a variety of products are prepared, in groups, possessing diversity in size, length, (molecular weight), and structural elements. These are then analyzed for the ability to bind specifically to an antibody, receptor, or other ligate.Type: GrantFiled: November 6, 2001Date of Patent: March 2, 2004Assignee: Space Hardware Optimization Technology, Inc.Inventors: John C. Vellinger, Paul W. Todd, Kenneth W. Barton, Scott Dunn, Mark S. Deuser
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Patent number: 6697793Abstract: A phrase generation is a method of generating sequences of terms, such as phrases, that may occur within a database of subsets containing sequences of terms, such as text. A database is provided and a relational model of the database is created. A query is then input. The query includes a term or a sequence of terms or multiple individual terms or multiple sequences of terms or combinations thereof. Next, several sequences of terms that are contextually related to the query are assembled from contextual relations in the model of the database. The sequences of terms are then sorted and output. Phrase generation can also be an iterative process used to produce sequences of terms from a relational model of a database.Type: GrantFiled: March 2, 2001Date of Patent: February 24, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Michael W. McGreevy
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Patent number: 6695251Abstract: A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) is connectable to the main thrust generator and at least one RCS controller is connectable to the RCS. The RCS controller and the TVC are synchronized to adjust the direction of the principal line of thrust through the body center of gravity.Type: GrantFiled: June 19, 2001Date of Patent: February 24, 2004Assignee: Space Systems/Loral, IncInventors: John J. Rodden, Andrew E. Turner
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Patent number: 6696943Abstract: A video monitoring system for use with a child car seat has video camera(s) mounted in the car seat. The video images are wirelessly transmitted to a remote receiver/display encased in a portable housing that can be removably mounted in the vehicle in which the car seat is installed.Type: GrantFiled: March 18, 2003Date of Patent: February 24, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Susan Vinz Elrod, Richard W. Dabney
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Patent number: 6696792Abstract: A compact plasma accelerator having components including a cathode electron source, an anodic ionizing gas source, and a magnetic field that is cusped. The components are held by an electrically insulating body having a central axis, a top axial end, and a bottom axial end. The cusped magnetic field is formed by a cylindrical magnet having an axis of rotation that is the same as the axis of rotation of the insulating body, and magnetized with opposite poles at its two axial ends; and an annular magnet coaxially surrounding the cylindrical magnet, magnetized with opposite poles at its two axial ends such that a top axial end has a magnetic polarity that is opposite to the magnetic polarity of a top axial end of the cylindrical magnet. The ionizing gas source is a tubular plenum that has been curved into a substantially annular shape, positioned above the top axial end of the annular magnet such that the plenum is centered in a ring-shaped cusp of the magnetic field generated by the magnets.Type: GrantFiled: August 8, 2002Date of Patent: February 24, 2004Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: John E. Foster
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Patent number: 6694898Abstract: A columnar race game having columns that move in a vertical direction. The object of the game is to hit a target causing actuation of the column in the vertical direction. The first column to reach a uppermost point activates a detection device which stops the game and signals the winner of the game.Type: GrantFiled: January 6, 2003Date of Patent: February 24, 2004Assignee: Bob's Space Racers, Inc.Inventor: Jack D. Cook, II