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  • Humans  (4)
  • Launch Vehicles and Launch Operations  (3)
  • Electronics and Electrical Engineering  (2)
  • Astronomy
  • Molecular Sequence Data
  • 2005-2009  (9)
  • 1925-1929
  • 2006  (9)
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  • 2005-2009  (9)
  • 1925-1929
Year
  • 1
    Publication Date: 2006-09-09
    Description: We used functional magnetic resonance imaging to demonstrate preserved conscious awareness in a patient fulfilling the criteria for a diagnosis of vegetative state. When asked to imagine playing tennis or moving around her home, the patient activated predicted cortical areas in a manner indistinguishable from that of healthy volunteers.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Owen, Adrian M -- Coleman, Martin R -- Boly, Melanie -- Davis, Matthew H -- Laureys, Steven -- Pickard, John D -- MC_U105559847/Medical Research Council/United Kingdom -- MC_U105580446/Medical Research Council/United Kingdom -- New York, N.Y. -- Science. 2006 Sep 8;313(5792):1402.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Medical Research Council Cognition and Brain Sciences Unit, Cambridge CB2 2EF, UK. adrian.owen@mrc-cbu.cam.ac.uk〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/16959998" target="_blank"〉PubMed〈/a〉
    Keywords: Adult ; *Awareness ; Brain/*physiopathology ; Brain Injuries/physiopathology/*psychology ; Brain Mapping ; *Consciousness ; Female ; Humans ; *Magnetic Resonance Imaging ; Neurons/physiology ; Persistent Vegetative State/physiopathology/*psychology
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 2
    Publication Date: 2006-11-18
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Spear, R C -- Seto, Edmund -- Remais, Justin -- Carlton, Elizabeth J -- Davis, George -- Qiu, Dongchuan -- Zhou, Xiaonong -- Liang, Song -- New York, N.Y. -- Science. 2006 Nov 17;314(5802):1081-3; author reply 1081-3.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/17110555" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Anti-Infective Agents/therapeutic use ; *Communicable Disease Control ; Fresh Water ; Humans
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 3
    Publication Date: 2006-08-05
    Description: Immunity-related p47 guanosine triphosphatases (IRG) play a role in defense against intracellular pathogens. We found that the murine Irgm1 (LRG-47) guanosine triphosphatase induced autophagy and generated large autolysosomal organelles as a mechanism for the elimination of intracellular Mycobacterium tuberculosis. We also identified a function for a human IRG protein in the control of intracellular pathogens and report that the human Irgm1 ortholog, IRGM, plays a role in autophagy and in the reduction of intracellular bacillary load.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Singh, Sudha B -- Davis, Alexander S -- Taylor, Gregory A -- Deretic, Vojo -- AI42999/AI/NIAID NIH HHS/ -- AI45148/AI/NIAID NIH HHS/ -- AI57831/AI/NIAID NIH HHS/ -- R01 AI057831/AI/NIAID NIH HHS/ -- T32 AI007538/AI/NIAID NIH HHS/ -- New York, N.Y. -- Science. 2006 Sep 8;313(5792):1438-41. Epub 2006 Aug 3.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Department of Molecular Genetics and Microbiology, University of New Mexico School of Medicine, Albuquerque, NM 87131, USA.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/16888103" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; *Autophagy ; Cell Line ; Cytosol/metabolism ; GTP-Binding Proteins/genetics/*physiology ; HeLa Cells ; Humans ; Interferon-gamma/immunology ; Lysosomes/metabolism/microbiology/ultrastructure ; Macrophages/*immunology/*microbiology ; Mice ; Microbial Viability ; Microtubule-Associated Proteins/metabolism ; Mycobacterium bovis/*immunology/physiology ; Phagosomes/metabolism/microbiology/*ultrastructure ; RNA, Small Interfering ; Transfection ; Vacuoles/metabolism/ultrastructure
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 4
    Publication Date: 2006-08-19
    Description: Congenital myasthenic syndromes (CMSs) are a group of inherited disorders of neuromuscular transmission characterized by fatigable muscle weakness. One major subgroup of patients shows a characteristic "limb girdle" pattern of muscle weakness, in which the muscles have small, simplified neuromuscular junctions but normal acetylcholine receptor and acetylcholinesterase function. We showed that recessive inheritance of mutations in Dok-7, which result in a defective structure of the neuromuscular junction, is a cause of CMS with proximal muscle weakness.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Beeson, David -- Higuchi, Osamu -- Palace, Jackie -- Cossins, Judy -- Spearman, Hayley -- Maxwell, Susan -- Newsom-Davis, John -- Burke, Georgina -- Fawcett, Peter -- Motomura, Masakatsu -- Muller, Juliane S -- Lochmuller, Hanns -- Slater, Clarke -- Vincent, Angela -- Yamanashi, Yuji -- G117/490/Medical Research Council/United Kingdom -- New York, N.Y. -- Science. 2006 Sep 29;313(5795):1975-8. Epub 2006 Aug 17.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Neurosciences Group, Weatherall Institute of Molecular Medicine, University of Oxford, John Radcliffe Hospital, Oxford OX3 9DS, UK. dbeeson@hammer.imm.ox.ac.uk〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/16917026" target="_blank"〉PubMed〈/a〉
    Keywords: Cell Line ; Cells, Cultured ; Female ; *Frameshift Mutation ; Genes, Recessive ; Humans ; Male ; Muscle Fibers, Skeletal/metabolism ; Muscle Proteins/*genetics/physiology ; Muscle Weakness/physiopathology ; Mutation ; Myasthenic Syndromes, Congenital/*genetics/pathology/physiopathology ; Neuromuscular Junction/*pathology/*physiopathology ; Pedigree ; Polymerase Chain Reaction ; Receptor Protein-Tyrosine Kinases/physiology ; Receptors, Cholinergic/metabolism/physiology ; Sequence Analysis, DNA ; Synaptic Transmission
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 5
    Publication Date: 2019-08-13
    Description: A video guidance sensor system for use, p.g., in automated docking of a chase vehicle with a target vehicle. The system includes an integrated rangefinder sub-system that uses time of flight measurements to measure range. The rangefinder sub-system includes a pair of matched photodetectors for respectively detecting an output laser beam and return laser beam, a buffer memory for storing the photodetector outputs, and a digitizer connected to the buffer memory and including dual amplifiers and analog-to-digital converters. A digital signal processor processes the digitized output to produce a range measurement.
    Keywords: Electronics and Electrical Engineering
    Format: application/pdf
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  • 6
    Publication Date: 2019-07-13
    Description: Options for development flight testing (DFT) of the Ares I Crew Launch Vehicle (CLV) are discussed. The Ares-I Crew Launch Vehicle (CLV) is being developed by the U.S. National Aeronautics and Space Administration (NASA) to launch the Crew Exploration Vehicle (CEV) into low Earth Orbit (LEO). The Ares-I implements one of the components of the Vision for Space Exploration (VSE), providing crew and cargo access to the International Space Station (ISS) after retirement of the Space Shuttle and, eventually, forming part of the launch capability needed for lunar exploration. The role of development flight testing is to demonstrate key sub-systems, address key technical risks, and provide flight data to validate engineering models in representative flight environments. This is distinguished from certification flight testing, which is designed to formally validate system functionality and achieve flight readiness. Lessons learned from Saturn V, Space Shuttle, and other flight programs are examined along with key Ares-I technical risks in order to provide insight into possible development flight test strategies. A strategy for the first test flight of the Ares I, known as Ares I-1, is presented.
    Keywords: Launch Vehicles and Launch Operations
    Type: 57th International Astronautical Congress (IAC 2006); Oct 02, 2006 - Oct 06, 2006; Valencia; Spain
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  • 7
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    In:  CASI
    Publication Date: 2019-07-13
    Description: The Agency s Crew Launch Vehicle (CLV) will be the first human rated space transportation system developed in the United States since the Space Shuttle. The CLV will utilize existing Shuttle heritage hardware and systems combined with a "clean sheet design" for the Upper Stage. The Upper Stage element will be designed and developed by a team of NASA engineers managed by the Marshall Space Flight Center (MSFC) in Huntsville, Alabama. The team will design the Upper Stage based on the Exploration Systems Architecture Study (ESAS) Team s point of departure conceptual design as illustrated in the figure below. This concept is a self-supporting cylindrical structure, approximately 1 15 feet long and 216 inches in diameter. While this "clean-sheet" upper stage design inherently carries more risk than utilizing a modified design, the approach also has many advantages. This paper will discuss the advantages and disadvantages of pursuing a "clean-sheet" design for the new CLV Upper Stage as well as describe in detail the overall design of the Upper Stage and its integration into NASA s CLV.
    Keywords: Launch Vehicles and Launch Operations
    Type: AIAA Joint Propulsion Conference; Jul 09, 2006 - Jul 12, 2006; Sacramento, CA; United States
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  • 8
    Publication Date: 2019-07-12
    Description: A single-chip CMOS-based (complementary-metal-oxide-semiconductorbased) transmit/receive (T/R) module is being developed for L-band radar systems. Previous T/R module implementations required multiple chips employing different technologies (GaAs, Si, and others) combined with off-chip transmission lines and discrete components including circulators. The new design eliminates the bulky circulator, significantly reducing the size and mass of the T/R module. Compared to multi-chip designs, the single-chip CMOS can be implemented with lower cost. These innovations enable cost-effective realization of advanced phased array and synthetic aperture radar systems that require integration of thousands of T/R modules. The circulator is a ferromagnetic device that directs the flow of the RF (radio frequency) power during transmission and reception. During transmission, the circulator delivers the transmitted power from the amplifier to the antenna, while preventing it from damaging the sensitive receiver circuitry. During reception, the circulator directs the energy from the antenna to the low-noise amplifier (LNA) while isolating the output of the power amplifier (PA). In principle, a circulator could be replaced by series transistors acting as electronic switches. However, in practice, the integration of conventional series transistors into a T/R chip introduces significant losses and noise. The prototype single-chip T/R module contains integrated transistor switches, but not connected in series; instead, they are connected in a shunt configuration with resonant circuits (see figure). The shunt/resonant circuit topology not only reduces the losses associated with conventional semiconductor switches but also provides beneficial transformation of impedances for the PA and the LNA. It provides full singlepole/ double-throw switching for the antenna, isolating the LNA from the transmitted signal and isolating the PA from the received signal. During reception, the voltage on control line RX/TX (raised bar) is high, causing the field-effect transistor (FET) switch S1 to be closed, forming a parallel resonant tank circuit L1||C1. This circuit presents high impedance to the left of the antenna, so that the received signal is coupled to the LNA. At the same time, FET switches S2 and S3 are open, so that C2 is removed from the circuit (except for a small parasitic capacitance). The combination of L2 and C3 forms a matching network that transforms the antenna impedance of 50 ohms to a higher value from the perspective of the LNA input terminal. This transformation of impedance improves LNA noise figure by increasing the received voltage delivered to the input transistor. This allows lower transconductance and therefore a smaller transistor, which makes it possible to design the CMOS LNA for low power consumption. During transmission, the voltage on control line RX/TX (raised bar) is low, causing switch S1 to be open. In this configuration, the combination of L1 and C1 transforms the antenna impedance to a lower value from the perspective of the PA. This low impedance is helpful in producing a relatively high output power compatible with the low CMOS operating potential. At the same time, switches S2 and S3 are closed, forming the parallel resonant tank circuit L2||C2. This circuit presents high impedance to the right of the antenna, directing the PA output signal to the antenna and away from the LNA. During this time, S3 presents a short circuit across the LNA input terminals to guarantee that the voltage seen by the LNA is small enough to prevent damage.
    Keywords: Electronics and Electrical Engineering
    Type: NPO-40869 , NASA Tech Briefs, April 2006; 11-12
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  • 9
    Publication Date: 2019-07-19
    Description: The Crew Launch Vehicle (CLV), a key component of NASA's blueprint for the next generation of spacecraft to take humans back to the moon, is being designed and built by engineers at NASA s Marshall Space Flight Center (MSFC). The vehicle s design is based on the results of NASA's 2005 Exploration Systems Architecture Study (ESAS), which called for development of a crew-launch system to reduce the gap between Shuttle retirement and Crew Exploration Vehicle (CEV) Initial Operating Capability, identification of key technologies required to enable and significantly enhance these reference exploration systems, and a reprioritization of near- and far-term technology investments. The Upper Stage Element (USE) of the CLV is a clean-sheet approach that is being designed and developed in-house, with element management at MSFC. The USE concept is a self-supporting cylindrical structure, approximately 115' long and 216" in diameter, consisting of the following subsystems: Primary Structures (LOX Tank, LH2 Tank, Intertank, Thrust Structure, Spacecraft Payload Adaptor, Interstage, Forward and Aft Skirts), Secondary Structures (Systems Tunnel), Avionics and Software, Main Propulsion System, Reaction Control System, Thrust Vector Control, Auxiliary Power Unit, and Hydraulic Systems. The ESAS originally recommended a CEV to be launched atop a four-segment Space Shuttle Main Engine (SSME) CLV, utilizing an RS-25 engine-powered upper stage. However, Agency decisions to utilize fewer CLV development steps to lunar missions, reduce the overall risk for the lunar program, and provide a more balanced engine production rate requirement prompted engineers to switch to a five-segment design with a single Saturn-derived J-2X engine. This approach provides for single upper stage engine development for the CLV and an Earth Departure Stage, single Reusable Solid Rocket Booster (RSRB) development for the CLV and a Cargo Launch Vehicle, and single core SSME development. While the RSRB design has changed since the CLV Project's inception, the USE design has remained essentially a clean-sheet approach. Although a clean-sheet upper stage design inherently carries more risk than a modified design, it does offer many advantages: a design for increased reliability; built-in extensibility to allow for commonality/growth without major redesign; and incorporation of state-of-the-art materials, hardware, and design, fabrication, and test techniques and processes to facilitate a potentially better, more reliable system. Because consideration was given in the ESAS to both clean-sheet and modified USE designs, this paper will highlight the advantages and disadvantages of both approaches and provide a detailed discussion of trades/selections made that led to the final upper stage configuration.
    Keywords: Launch Vehicles and Launch Operations
    Type: 57th International Astronautical Congress; Oct 02, 2006 - Oct 06, 2006; Valencia; Spain
    Format: text
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