Patents Assigned to Space
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Publication number: 20040031618Abstract: The invention discloses a method for making two sided Multi-Chip Modules (MCMs) that will allow most commercially available integrated circuits to meet the thermal and radiation hazards of the spacecraft environment using integrated package shielding technology. The invention describes the technology and methodology to manufacture MCMs that are radiation-hardened, structurally and thermally stable using 3-dimensional techniques allowing for high density integrated circuit packaging in a radiation hardened package.Type: ApplicationFiled: August 18, 2003Publication date: February 19, 2004Applicants: Maxwell Electronic Components Group, Inc., Space Electronics, Inc.Inventors: David R. Czjakowski, Neil Eggleston, Janet S. Patterson
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Patent number: 6691955Abstract: A momentum wheel configuration that may be used on a spacecraft having a momentum bias that prevents zero wheel speeds. The momentum wheel configuration comprises three or more momentum wheels. The momentum wheels are oriented such that their wheel axes are not parallel to each other. The momentum wheels are oriented such that their axial momentum vectors are not coplanar. None of the momentum wheels have their wheel axis parallel to the momentum bias direction of the spacecraft. No two of the momentum wheels are oriented such that their axial momentum vectors are coplanar with the momentum bias direction of the spacecraft.Type: GrantFiled: November 27, 2001Date of Patent: February 17, 2004Assignee: Space Systems/LoralInventors: Keith Reckdahl, Xenophon Price
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Patent number: 6689952Abstract: A large membrane space structure deployed and spanned by centrifugal force owing to the spin motion, contains a hub located at a central portion thereof and a sail including a plurality of petals attached to the hub by supports. Each of the petals has regions symmetrical to an imaginary center line passing through the center of the hub. Membranes are spanned on the regions. Each of the membranes is divided into parts of suitable shapes, and adjacent membranes are discretely connected to each other by bridge belts to suppress the residual crease strain. The petals are symmetric with respect to the center of the hub. Deployment force is provided in the circumferential direction by the introduction of imaginary tension lines. The petals may be connected to each other to help deployment.Type: GrantFiled: December 14, 2001Date of Patent: February 10, 2004Assignee: The Director-General of the Institute of Space and Astronautical ScienceInventor: Junichiro Kawaguchi
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Patent number: 6689288Abstract: The invention described herein supplies a new class of electroactive polymeric blend materials which offer both sensing and actuation dual functionality. The blend comprises two components, one component having a sensing capability and the other component having an actuating capability. These components should be co-processable and coexisting in a phase separated blend system. Specifically, the materials are blends of a sensing component selected from the group consisting of ferroelectric, piezoelectric, pyroelectric and photoelectric polymers and an actuating component that responds to an electric field in terms of dimensional change. Said actuating component includes, but is not limited to, electrostrictive graft elastomers, dielectric electroactive elastomers, liquid crystal electroactive elastomers and field responsive polymeric gels. The sensor functionality and actuation functionality are designed by tailoring the relative fraction of the two components.Type: GrantFiled: November 28, 2001Date of Patent: February 10, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Terry L. St. Clair, Joycelyn S. Harrison, Ji Su, Zoubeida Ounaies
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Patent number: 6690934Abstract: A shared single system of ground stations (120) for servicing any number of satellite owners, permits the owners to transfer command information to their satellite (110), and collect data streams that arm sent back from the satellite all via a standardized global communication system maintained and operated by a commercial satellite communications company. A remotely controlled ground station (120) is operated and controlled from a central controller. Each user creates and stores a ground station configuration file at the central controller, which file contains the data necessary to configure the remotely controlled ground station (120) to communicate with the user's satellite (110). When the user desires to communicate with the user's satellite, the user schedules a communication session with the central controller, which downloads the configuration file to the appropriate ground station.Type: GrantFiled: June 5, 2000Date of Patent: February 10, 2004Assignee: Universal Space Network, Inc.Inventors: Charles Conrad, Jr., Thomas Ray Ingersoll, Carl Joseph Glim, David Earl Massey
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Publication number: 20040020115Abstract: The present invention provides a micro gravity environmental control apparatus, such as a plant cultivating apparatus, an animal raising apparatus, and a micro gravity environmental control method, such as a plant cultivating method, an animal raising method, a breeding method, capable of cultivating a plant and raising an animal by using soil and also capable of recovering moisture supplied to the soil so as to reuse the moisture, under a weightless environment or a micro gravity environment. There is provided a micro gravity environmental control apparatus comprising a chamber, an air suction pipe arranged in the vicinity of a lower end portion within the chamber, and an air sucking part communicated and connected with the air suction pipe and used for sucking air within the chamber out of the chamber.Type: ApplicationFiled: April 24, 2003Publication date: February 5, 2004Applicants: National Agricultural Research Organization, The National Space Development Agency of Japan, The Japan Space Forum (a Japan Foundation)Inventors: Masayuki Hirafuji, Tokihiro Fukatsu, Kei Tanaka, Keiko Ibaraki
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Patent number: 6685136Abstract: A pressure-resistant balloon includes a gasbag and a volume changing mechanism which deforms the gasbag in a fully inflated state to change a volume of the gasbag. The gasbag includes spindle-shaped gores of an airtight film material, adjacent gores joined together at side edges, and load tapes fitted to joined sections of the side edges, and extending along the side edges, respectively. After inflated, the gasbag allows no gas to be discharged so as to maintain an internal gas pressure. Each of the gores outwardly protrudes between two adjacent load tapes without an elongation of the airtight film material of the gore, when the gasbag is in the fully inflated state. The protruding gore has a radius of curvature in a direction intersecting with the two adjacent load tapes. The radius of curvature is smaller than a radius of the gasbag.Type: GrantFiled: November 6, 2002Date of Patent: February 3, 2004Assignee: The Director-General of the Institute of Space and Astronautical ScienceInventors: Nobuyuki Yajima, Naoki Izutsu, Hideyuki Honda
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Patent number: 6684940Abstract: The performance of a heat pipe system is greatly improved by the use of a dilute aqueous solution of about 0.0005 and about 0.005 moles per liter of a long chain alcohol as the working fluid. The surface tension-temperature gradient of the long-chain alcohol solutions turns positive as the temperature exceeds a certain value, for example about 40° C. for n-heptanol solutions. Consequently, the Marangoni effect does not impede, but rather aids in bubble departure from the heating surface. Thus, the bubble size at departure is substantially reduced at higher frequencies and, therefore, increases the boiling limit of heat pipes. This feature is useful in microgravity conditions. In addition to microgravity applications, the heat pipe system may be used for commercial, residential and vehicular air conditioning systems, micro heat pipes for electronic devices, refrigeration and heat exchangers, and chemistry and cryogenics.Type: GrantFiled: May 29, 2002Date of Patent: February 3, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David F. Chao, Nengli Zhang
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Patent number: 6684724Abstract: A shape memory alloy step drive mechanism includes at least one shape memory alloy element (1) with a fixed end, the other end being connected to one end of a lever (2). The lever (2) is provided with a pawl (4) which is located to move on the teeth of a ratchet wheel (5) mounted on a main shaft (6) along with the lever (2). A stopper pin (7) is provided which also guides the pawl (4) on the ratchet wheel (5). A bias spring (9) is provided on a mandril on the main shaft (6) for returning the lever (2) to its original position. A detent wheel (8) with at least one detent lever (10) is mounted on the main shaft (6) to provide the detent torque required to hold the main shaft (6) in position when the lever (2) returns to its original position. A pair of support brackets (11) are provided for supporting and holding the various components together in an assembly.Type: GrantFiled: October 16, 2001Date of Patent: February 3, 2004Assignee: Indian Space Research OrganizationInventors: Viswanatha Narasimhiah, Murali Parathasarathy Iyengar Talkao
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Patent number: 6684695Abstract: A mass flow sensor to be mounted within a duct and measures the mass flow of a fluid stream moving through the duct. The sensor is an elongated thin quartz substrate having a plurality of platinum strips extending in a parallel relationship on the strip, with certain of the strips being resistors connected to an excitation voltage. The resistors form the legs of a Wheatstone bridge. The resistors are spaced a sufficient distance inwardly from the leading and trailing edges of the substrate to lie within the velocity recovery region so that the measured flow is the same as the actual upstream flow. The resistor strips extend at least half-way through the fluid stream to include a substantial part of the velocity profile of the stream. Certain of the resistors detect a change in temperature as the fluid stream moves across the substrate to provide an output signal from the Wheatstone bridge which is representative of the fluid flow.Type: GrantFiled: October 8, 2002Date of Patent: February 3, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Gustave C. Fralick, Danny P. Hwang, John D. Wrbanek
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Publication number: 20040016477Abstract: A magnetic alloy raw material is heated and melted to create a melt with floating said raw material by means of electromagnetic field from an inductive type heating coil. The melt is located in between a pair of cupper cooling plates driven by a solenoid coil, and then, splat-cooled below the peritectic point of the raw material by the cooling plates.Type: ApplicationFiled: March 26, 2003Publication date: January 29, 2004Applicant: The Institute of Space and Astronautical ScienceInventor: Kazuhiko Kuribayashi
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Publication number: 20040019415Abstract: A stratospheric flying object which is placed in the stratosphere of the earth has an airship-shaped flying object body, a despun platform unit mounted on the flying object body by a mount, and a controller for detecting an azimuthal angle of the despun platform unit in a horizontal plane and controlling the platform unit to face in a constant direction at all times within the horizontal plane. Preferably, directional antennas and telescopes for optical communications are mounted on the despun platform unit.Type: ApplicationFiled: July 17, 2003Publication date: January 29, 2004Applicant: NEC Toshiba Space Systems, Ltd.Inventors: Toshinori Hotta, Wakoto Akinaga
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Patent number: 6682418Abstract: A game in which a player shoots water, air, light, a missile, or any other suitable projectile at a target. The target is activated when it is hit by the projectile. Activation of the target causes a plurality of lights to emit light in a predetermined order. The player wins the game by causing all of the lights to emit light.Type: GrantFiled: October 6, 2000Date of Patent: January 27, 2004Assignee: Bob's Space Racers, Inc.Inventors: John F. Mendes, Weimar P. Tudela, David A. Wise
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Patent number: 6680797Abstract: A polarization-independent optical switch is disclosed for switching at least one incoming beam from at least one input source to at least one output drain.Type: GrantFiled: June 21, 2001Date of Patent: January 20, 2004Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventor: Richard D. Juday
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Publication number: 20040009090Abstract: To provide a nickel based brazing filler metal which does not contain at all boron (B) or phosphorus (P) that is likely to form a hard and brittle compound in the brazed layer, in which the liquidus is lowered below 1,100° C. by adding a small amount of silicon (Si) and is abundant in ductility, heat-resistance and corrosion resistance. This is attained by a nickel based brazing filler metal characterized by containing manganese (Mn) of 13 to 20% by wt. and silicon (Si) of 5 to 7% by wt. added as melting point depression elements and chrome (Cr) of 16 to 21% by wt. and the balance consisting of nickel (Ni) and the impurities.Type: ApplicationFiled: July 10, 2003Publication date: January 15, 2004Applicants: NATIONAL SPACE DEVELOPMENT AGENCY OF JAPAN, THE JAPAN WELDING ENGINEERING SOCIETYInventors: Makoto Shirai, Ken Sasabe, Takehiko Watanabe
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Publication number: 20040009605Abstract: A means for detecting volatile organic compounds which utilizes a catalytic material to oxidize volatile organic compounds at temperatures substantially lower than the autoignition temperature of the compound. Because this reaction is exothermic, a thermistor in contact with the catalytic material is used to detect the heat evolved as volatile organic compounds are oxidized to carbon dioxide and water at the catalyst surface. Upon comparison to a reference thermistor, relative increases in the temperature of the sensing thermistor correspond positively with an increased concentration of volatile organic compounds and are thus used as an indicator of the presence of such compounds.Type: ApplicationFiled: June 20, 2003Publication date: January 15, 2004Applicant: U.S. as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Kenneth G. Brown, Donald M. Oglesby, Bradley D. Leighty, Erik J. Kielin, David R. Schryer, Billy T. Upchurch
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Patent number: 6677761Abstract: Wiring defects are located by detecting a reflected signal that is developed when an arc occurs through the defect to a nearby ground. The time between the generation of the signal and the return of the reflected signal provides an indication of the distance of the arc (and therefore the defect) from the signal source. To ensure arcing, a signal is repeated at gradually increasing voltages while the wire being tested and a nearby ground are immersed in a conductive medium. In order to ensure that the arcing occurs at an identifiable time, the signal whose reflection is to be detected is always made to reach the highest potential yet seen by the system.Type: GrantFiled: December 12, 2001Date of Patent: January 13, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Owen R. Greulich
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Patent number: 6676288Abstract: A process for thermal imaging scanning of a swaged heater of an anode subassembly of a hollow cathode assembly, comprising scanning a swaged heater with a thermal imaging radiometer to measure a temperature distribution of the heater; raising the current in a power supply to increase the temperature of the swaged heater; and measuring the swaged heater temperature using the radiometer, whereupon the temperature distribution along the length of the heater shall be less than plus or minus 5 degrees C.Type: GrantFiled: August 8, 2002Date of Patent: January 13, 2004Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventors: Michael J. Patterson, Timothy R. R. Verhey, George C. Soulas
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Patent number: 6676964Abstract: Microcapsules prepared by encapsulating an aqueous solution of a protein, drug or other bioactive substance inside a semi-permeable membrane by are disclosed. The microcapsules are formed by interfacial coacervation under conditions where the shear forces are limited to 0-100 dynes/cm2 at the interface. By placing the microcapsules in a high osmotic dewatering solution, the protein solution is gradually made saturated and then supersaturated, and the controlled nucleation and crystallization of the protein is achieved. The crystal-filled microcapsules prepared by this method can be conveniently harvested and stored while keeping the encapsulated crystals in essentially pristine condition due to the rugged, protective membrane. Because the membrane components themselves are x-ray transparent, large crystal-containing microcapsules can be individually selected, mounted in x-ray capillary tubes and subjected to high energy x-ray diffraction studies to determine the 3-D structure of the protein molecules.Type: GrantFiled: January 26, 2001Date of Patent: January 13, 2004Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventors: Dennis R. Morrison, Benjamin Mosier
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Patent number: 6676912Abstract: A method for removing NOX from gas streams emanating from stationary combustion sources and manufacturing plants utilizes the injection of hydrogen peroxide into the gas stream for rapid gas-phase oxidation of NO to NO2 and water-soluble nitrogen acids HNO2 and HNO3. The nitrogen acids may be removed from the oxidized gas stream by wet scrubbing or by contact with a particulate alkaline material to form a nitrite/nitrate salt.Type: GrantFiled: October 27, 2000Date of Patent: January 13, 2004Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventors: Charles D. Cooper, Christian A. Clausen, III, Michelle M. Collins