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  • Mice  (1,374)
  • Spacecraft Design, Testing and Performance  (864)
  • 2005-2009  (2,238)
  • 1
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    Zero-Propellant Maneuver[TM] Flight Results for 180 deg ISS Rotation (2007)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: This paper presents results for the Zero Propellant Maneuver (ZPM) TradeMark attitude control concept flight demonstration. On March 3, 2007, a ZPM was used to reorient the International Space Station 180 degrees without using any propellant. The identical reorientation performed with thrusters would have burned 110lbs of propellant. The ZPM was a pre-planned trajectory used to command the CMG attitude hold controller to perform the maneuver between specified initial and final states while maintaining the CMGs within their operational limits. The trajectory was obtained from a PseudoSpectral solution to a new optimal attitude control problem. The flight test established the breakthrough capability to simultaneously perform a large angle attitude maneuver and momentum desaturation without the need to use thrusters. The flight implementation did not require any modifications to flight software. This approach is applicable to any spacecraft that are controlled by momentum storage devices.
    Keywords: Spacecraft Design, Testing and Performance
    Type: Proceedings of the 20th International Symposium on Space Flight Dynamics; NASA/CP-2007-214158
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  • 2
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    Zero to Integration in Eight Months, the Dawn Ground Data System Engineering Challange (2006)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: The Dawn Project has presented the Ground Data System (GDS) with technical challenges driven by cost and schedule constraints commonly associated with National Aeronautics and Space Administration (NASA) Discovery Projects. The Dawn mission consists of a new and exciting Deep Space partnership among: the Jet Propulsion Laboratory (JPL), responsible for project management and flight operations; Orbital Sciences Corporation (OSC), spacecraft builder and responsible for flight system test and integration; and the University of California, at Los Angeles (UCLA), responsible for science planning and operations. As a cost-capped mission, one of Dawn s implementation strategies is to leverage from both flight and ground heritage. OSC's ground data system is used for flight system test and integration as part of the flight heritage strategy. Mission operations, however, are to be conducted with JPL s ground system. The system engineering challenge of dealing with two heterogeneous ground systems emerged immediately. During the first technical interchange meeting between the JPL s GDS Team and OSC's Flight Software Team, August 2003, the need to integrate the ground system with the flight software was brought to the table. This need was driven by the project s commitment to enable instrument engineering model integration in a spacecraft simulator environment, for both demonstration and risk mitigation purposes, by April 2004. This paper will describe the system engineering approach that was undertaken by JPL's GDS Team in order to meet the technical challenge within a non-negotiable eight-month schedule. Key to the success was adherence to an overall systems engineering process and fundamental systems engineering practices: decomposition of the project request into manageable requirements; definition of a structured yet flexible development process; integration of multiple ground disciplines and experts into a focused team effort; in-process risk management; and aggregation of the intermediate products to an integrated final product. In addition, this paper will highlight the role of lessons learned from the integration experience. The lessons learned from an early GDS deployment have served as the foundation for the design and implementation of the Dawn Ground Data System.
    Keywords: Spacecraft Design, Testing and Performance
    Type: SpaceOps Conference; 19-23 Ju. 2006; Rome; Italy
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  • 3
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    Zc3h12a is an RNase essential for controlling immune responses by regulating mRNA decay (2009)
    Nature Publishing Group (NPG)
    Details
    Publication Date: 2009-03-27
    Description: Toll-like receptors (TLRs) recognize microbial components, and evoke inflammation and immune responses. TLR stimulation activates complex gene expression networks that regulate the magnitude and duration of the immune reaction. Here we identify the TLR-inducible gene Zc3h12a as an immune response modifier that has an essential role in preventing immune disorders. Zc3h12a-deficient mice suffered from severe anaemia, and most died within 12 weeks. Zc3h12a(-/-) mice also showed augmented serum immunoglobulin levels and autoantibody production, together with a greatly increased number of plasma cells, as well as infiltration of plasma cells to the lung. Most Zc3h12a(-/-) splenic T cells showed effector/memory characteristics and produced interferon-gamma in response to T-cell receptor stimulation. Macrophages from Zc3h12a(-/-) mice showed highly increased production of interleukin (IL)-6 and IL-12p40 (also known as IL12b), but not TNF, in response to TLR ligands. Although the activation of TLR signalling pathways was normal, Il6 messenger RNA decay was severely impaired in Zc3h12a(-/-) macrophages. Overexpression of Zc3h12a accelerated Il6 mRNA degradation via its 3'-untranslated region (UTR), and destabilized RNAs with 3'-UTRs for genes including Il6, Il12p40 and the calcitonin receptor gene Calcr. Zc3h12a contains a putative amino-terminal nuclease domain, and the expressed protein had RNase activity, consistent with a role in the decay of Il6 mRNA. Together, these results indicate that Zc3h12a is an essential RNase that prevents immune disorders by directly controlling the stability of a set of inflammatory genes.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Matsushita, Kazufumi -- Takeuchi, Osamu -- Standley, Daron M -- Kumagai, Yutaro -- Kawagoe, Tatsukata -- Miyake, Tohru -- Satoh, Takashi -- Kato, Hiroki -- Tsujimura, Tohru -- Nakamura, Haruki -- Akira, Shizuo -- P01 AI070167/AI/NIAID NIH HHS/ -- England -- Nature. 2009 Apr 30;458(7242):1185-90. doi: 10.1038/nature07924. Epub 2009 Mar 25.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Laboratory of Host Defense, WPI Immunology Frontier Research Center, Osaka University, 3-1 Yamada-oka, Suita, Osaka 565-0871, Japan.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/19322177" target="_blank"〉PubMed〈/a〉
    Keywords: 3' Untranslated Regions/genetics/metabolism ; Anemia/complications/genetics ; Animals ; Autoantibodies/blood/immunology ; Autoimmune Diseases/complications/immunology ; Cell Line ; Cytokines/biosynthesis/genetics ; Fetal Diseases/immunology ; Humans ; Immunity/*genetics/*immunology ; Inflammation Mediators/metabolism ; Interleukin-6/genetics ; Macrophages, Peritoneal/immunology/metabolism ; Mice ; Plasma Cells/cytology ; *RNA Stability ; Ribonucleases/deficiency/genetics/*metabolism ; T-Lymphocytes/immunology
    Print ISSN: 0028-0836
    Electronic ISSN: 1476-4687
    Topics: Biology , Chemistry and Pharmacology , Medicine , Natural Sciences in General , Physics
    Published by Nature Publishing Group (NPG)
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  • 4
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    XIAP discriminates between type I and type II FAS-induced apoptosis (2009)
    Nature Publishing Group (NPG)
    Details
    Publication Date: 2009-07-25
    Description: FAS (also called APO-1 and CD95) and its physiological ligand, FASL, regulate apoptosis of unwanted or dangerous cells, functioning as a guardian against autoimmunity and cancer development. Distinct cell types differ in the mechanisms by which the 'death receptor' FAS triggers their apoptosis. In type I cells, such as lymphocytes, activation of 'effector caspases' by FAS-induced activation of caspase-8 suffices for cell killing, whereas in type II cells, including hepatocytes and pancreatic beta-cells, caspase cascade amplification through caspase-8-mediated activation of the pro-apoptotic BCL-2 family member BID (BH3 interacting domain death agonist) is essential. Here we show that loss of XIAP (X-chromosome linked inhibitor of apoptosis protein) function by gene targeting or treatment with a second mitochondria-derived activator of caspases (SMAC, also called DIABLO; direct IAP-binding protein with low pI) mimetic drug in mice rendered hepatocytes and beta-cells independent of BID for FAS-induced apoptosis. These results show that XIAP is the critical discriminator between type I and type II apoptosis signalling and suggest that IAP inhibitors should be used with caution in cancer patients with underlying liver conditions.〈br /〉〈br /〉〈a href="https://www.ncbi.nlm.nih.gov/pmc/articles/PMC2956120/" target="_blank"〉〈img src="https://static.pubmed.gov/portal/portal3rc.fcgi/4089621/img/3977009" border="0"〉〈/a〉   〈a href="https://www.ncbi.nlm.nih.gov/pmc/articles/PMC2956120/" target="_blank"〉This paper as free author manuscript - peer-reviewed and accepted for publication〈/a〉〈br /〉〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Jost, Philipp J -- Grabow, Stephanie -- Gray, Daniel -- McKenzie, Mark D -- Nachbur, Ueli -- Huang, David C S -- Bouillet, Philippe -- Thomas, Helen E -- Borner, Christoph -- Silke, John -- Strasser, Andreas -- Kaufmann, Thomas -- CA 43540/CA/NCI NIH HHS/ -- CA 80188/CA/NCI NIH HHS/ -- R01 CA043540/CA/NCI NIH HHS/ -- R01 CA043540-09/CA/NCI NIH HHS/ -- R01 CA043540-22/CA/NCI NIH HHS/ -- R01 CA080188-01/CA/NCI NIH HHS/ -- R01 CA080188-08/CA/NCI NIH HHS/ -- England -- Nature. 2009 Aug 20;460(7258):1035-9. doi: 10.1038/nature08229. Epub 2009 Jul 22.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉The Walter and Eliza Hall Institute of Medical Research, Melbourne University, Parkville, Victoria 3050, Australia.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/19626005" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Antigens, CD95/antagonists & inhibitors/immunology/*metabolism ; *Apoptosis ; BH3 Interacting Domain Death Agonist Protein/deficiency/genetics ; Biomimetic Materials/pharmacology ; Caspase Inhibitors ; Enzyme Activation ; Fas Ligand Protein/metabolism ; Female ; Hepatitis/metabolism/pathology ; Hepatocytes/cytology/drug effects/metabolism ; Male ; Mice ; Mice, Inbred C57BL ; Signal Transduction ; Thymus Gland/cytology/drug effects ; X-Linked Inhibitor of Apoptosis Protein/antagonists & ; inhibitors/deficiency/genetics/*metabolism
    Print ISSN: 0028-0836
    Electronic ISSN: 1476-4687
    Topics: Biology , Chemistry and Pharmacology , Medicine , Natural Sciences in General , Physics
    Published by Nature Publishing Group (NPG)
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  • 5
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    Xenia Spacecraft Study (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: This slide presentation reviews the proposed design for the Xenia mission spacecraft. The goal of this study is to perform a mission concept study for the mission. Included in this study are: the overall ground rules and assumptions (GR&A), a mission analysis, the configuration, the mass properties, the guidance, Navigation and control, the proposed avionics, the power system, the thermal protection system, the propulsion system, and the proposed structures. Conclusions from the study indicate that the observatory fits within the Falcon 9 mass and volume envelope for launching from Omelek, the pointing, slow slewing, and fast slewing requirements and the thermal requirements are met.
    Keywords: Spacecraft Design, Testing and Performance
    Type: M09-0347
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  • 6
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    Xenia Spacecraft Study (2008)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: This slide presentation reviews the mission concept for the proposed Xenia mission. The mission's ground rules and assumptions for the mission analysis, attitude and orbit control, propulsion, avionics, power, and the thermal controls are reviewed, partially to determine the appropriate launch vehicle that will be used. A current design plan for the mission is shown assuming 6 GRB detectors and estimates for structures are reviewed.
    Keywords: Spacecraft Design, Testing and Performance
    Type: M09-0107
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  • 7
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    Xenia Mission: Spacecraft Design Concept (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: The proposed Xenia mission will, for the first time, chart the chemical and dynamical state of the majority of baryonic matter in the universe. using high-resolution spectroscopy, Xenia will collect essential information from major traces of the formation and evolution of structures from the early universe to the present time. The mission is based on innovative instrumental and observational approaches: observing with fast reaction gamma-ray bursts (GRBs) with a high spectral resolution. This enables the study of their (star-forming) environment from the dark to the local universe and the use of GRBs as backlight of large-scale cosmological structures, observing and surveying extended sources with high sensitivity using two wide field-of-view x-ray telescopes - one with a high angular resolution and the other with a high spectral resolution.
    Keywords: Spacecraft Design, Testing and Performance
    Type: NASA/TM-2009-216270 , M-1272
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  • 8
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    X-43D Conceptual Design and Feasibility Study (2005)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: NASA s Next Generation Launch Technology (NGLT) Program, in conjunction with the office of the Director of Defense Research and Engineering (DDR&E), developed an integrated hypersonic technology demonstration roadmap. This roadmap is an integral part of the National Aerospace Initiative (NAI), a multi-year, multi-agency cooperative effort to invest in and develop, among other things, hypersonic technologies. This roadmap contains key ground and flight demonstrations required along the path to developing a reusable hypersonic space access system. One of the key flight demonstrations required for systems that will operate in the high Mach number regime is the X-43D. As currently conceived, the X-43D is a Mach 15 flight test vehicle that incorporates a hydrogen-fueled scramjet engine. The purpose of the X-43D is to gather high Mach number flight environment and engine operability information which is difficult, if not impossible, to gather on the ground. During 2003, the NGLT Future Hypersonic Flight Demonstration Office initiated a feasibility study on the X-43D. The objective of the study was to develop a baseline conceptual design, assess its performance, and identify the key technical issues. The study also produced a baseline program plan, schedule, and cost, along with a list of key programmatic risks.
    Keywords: Spacecraft Design, Testing and Performance
    Type: AIAA Paper 2005-3416 , 13th AIAA/CIRA International Space Planes and Hypersonic Systems Technologies Conference; May 16, 2005 - May 20, 2005; Capua; Italy
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  • 9
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    X-43A Project Overview: Adventures in Hypersonics (2007)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: This viewgraph presentation gives a general overview of the X-43A program. The contents include: 1) X-43A Program Overview; 2) Vehicle Description; 3) Flight 1, MIB & Return to Flight; 4) Flight 2 and Results; and 5) Flight 3 and Results.
    Keywords: Spacecraft Design, Testing and Performance
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  • 10
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    X-43A Project Overview: Adventures in Hypersonics (2007)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: A viewgraph presentation describing the hypersonics program at NASA Dryden Flight Research Center is shown. The topics include: 1) X-43A Program Overview; 2) Vehicle Description; 3) Flight 1, MIB & Return to Flight; 4) Flight 2 and Results; 5) Flight 3 and Results; and 6) Concluding Remarks
    Keywords: Spacecraft Design, Testing and Performance
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