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  • Genetics  (4)
  • Spacecraft Design, Testing and Performance  (3)
  • Purification
  • 1995-1999  (9)
  • 1985-1989
  • 1998  (7)
  • 1995  (2)
  • 1
    ISSN: 0749-503X
    Keywords: LFH deletion cassette ; functional analysis ; chromosome IV ; Saccharomyces cerevisiae ; Life and Medical Sciences ; Genetics
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology
    Notes: We report here the construction of six deletion mutants and the analysis of their basic phenotype. Deletion cassettes containing the KanMX4 marker module and long flanking regions homologous to the target locus were constructed for each of the six open reading-frames (ORFs YDL088c, YDL087c, YDL086w, YDL085w, YDL084w and YDL082w) located on chromosome IV. Sporulation and tetrad analysis of heterozygous deletant strains revealed that, in the FY1679 genetic background, ORFs YDL088c, YDL087c and YDL084w are essential genes for vegetative growth whereas YDL086w, YDL085w and YDL082w are non-essential. ydl088cΔ and ydl084wΔ haploid strains are viable in the CEN. PK2 genetic background although ydl084wΔ grows at a slower rate than the wild type. Complementation tests by corresponding cognate genes confirmed that gene inactivation was responsible for these growth defects. © 1998 John Wiley & Sons, Ltd.
    Additional Material: 1 Ill.
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  • 2
    ISSN: 0749-503X
    Keywords: Saccharomyces cerevisiae ; chromosome VII ; ribonuclease PH ; HGH1 ; YGR187c ; YGR189c ; YGR194c ; YGR195w ; YGR196c ; YGR198w ; Life and Medical Sciences ; Genetics
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology
    Notes: We have deleted six different ORFs of unknown function located on the right arm of Saccharomyces cerevisiae chromosome VII; namely, YGR187c/HGH1, YGR189c, YGR194c, YGR195w, YGR196c and YGR198w. No basic phenotypes could be attributed to the strains deleted in any of genes YGR187c/HGH1, YGR189c, YGR194c and YGR196c. These deletants did not show mating, sporulation or growth defects under any of the conditions tested. However, spores bearing deletions in either the YGR195w or YGR198w genes were unable to develop into macroscopical colonies. The YGR195w gene product shows significant homology with bacterial ribonuclease PH, an enzyme hitherto undescribed in yeasts, and its deletion causes a loss of viability after one to three rounds of cell division. Overexpression of this gene, using a tetracycline-regulatable promoter system, did not cause any effect on the cells. Contrary to what has been reported for prokaryotic homologs, this enzyme could play an essential role in yeast cell biology. The product encoded by the other essential ORF, YGR198w, shows no significant homology with any protein of known function in the databases. Spores bearing the deletion usually germinate and give rise to microcolonies of 50-100 non-viable cells. © 1998 John Wiley & Sons, Ltd.
    Additional Material: 2 Ill.
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  • 3
    Electronic Resource
    Electronic Resource
    New York, NY [u.a.] : Wiley-Blackwell
    Yeast 11 (1995), S. 425-433 
    ISSN: 0749-503X
    Keywords: Yarrowia lipolytica ; orotate phosphoribosyl transferase ; nucleotide sequence ; transcription ; Life and Medical Sciences ; Genetics
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology
    Notes: The URA5 gene of Yarrowia lipolytica encoding the orotate phosphoribosyl transferase (OPRTase, EC2.4.2.10) was isolated by target integration in a mutant strain originally named ura2.21. The nucleotide sequence of the gene predicts a protein with high similarities with the OPRTases from Saccharomyces cerevisiae, Podospora anserina and Escherichia coli and to a lesser extent with that of Dictyostelium discoideum. The transcription start point has been mapped by primer extension analysis and indicates the existence of a long leader sequence in the corresponding mRNA. Northern-blot hybridization revealed the URA5 transcript to be approximately 0·94 kb. Deletion of the URA5 gene in Y. lipolytica produced a leaky phenotype similar to the one described for the ura5 mutation in S. cerevisiae. The URA5 gene of Y. lipolytica was able to complement functionally the ura5 mutation of S. cerevisiae. The sequence presented here has been submitted to the EMBL data library under Accession Number Z22571.
    Additional Material: 10 Ill.
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  • 4
    ISSN: 0749-503X
    Keywords: yeast genome ; chromosome VII ; histidine permease ; glyceraldehyde-3-phosphate dehydrogenase ; pyruvate dehydrogenase ; Life and Medical Sciences ; Genetics
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology
    Notes: We report the sequence of a 9037 bp fragment from the right arm of Saccharomyces cerevisiae chromosome VII. Analysis of the sequence revealed four complete open reading frames (ORFs), namely G7572, G7576, G7579 and G7584. The first three corresponded, respectively, to the previously cloned genes: HIP1, coding for a high-affinity histidine-specific permease, TDH1, one of the known genes coding for glyceraldehyde-3-phosphate dehydrogenase and ODPX, which encodes a precursor of protein X, a component of the pyruvate dehydrogenase complex. The ORF G7584 showed 35·8% identity with a hypothetical protein of Caenorhabditis elegans chromosome 3. The reported sequence has been deposited in the EMBL data library under Accession Number X82408.
    Additional Material: 2 Ill.
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  • 5
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Electrophoresis 19 (1998), S. 1117-1126 
    ISSN: 0173-0835
    Keywords: Purification ; Free-flow electrophoresis ; Transport phenomena ; Chemistry ; Biochemistry and Biotechnology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Chemistry and Pharmacology
    Notes: Free-flow zone electrophoresis may be used to purify biological samples, due to differences in electrophoretic mobility, in absence of a matrix - most frequently a gel - thus enabling the biological integrity of even fragile molecules to be preserved. However, the process is more complicated than its principle suggests due to different transport phenomena interfering with electrophoretic migration, with the resultant separation depending both on separation effects and dispersive phenomena. The physical origin of the main effects involved was identified. Mathematical expressions were proposed to estimate the influence of the crescent effect and electrohydrodynamics on the process. In this paper, these equations are used to determine the minimum difference in electrophoretic mobility required for a separation to be achieved with respect to the processing parameters. A methodology is proposed which defines the conditions under which the difference in electrophoretic mobilities equals that calculated when considering the influence of dispersive phenomena. Optimized separations of the whey proteins lactoferrin and albumin, known to interact strongly, and the purification of a monoclonal antibody from a mouse ascitic fluid illustrate the approach.
    Additional Material: 15 Ill.
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  • 6
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Electrophoresis 19 (1998), S. 1294-1299 
    ISSN: 0173-0835
    Keywords: Isoelectric focusing ; Continuous free flow electrophoresis ; Purification ; Chemistry ; Biochemistry and Biotechnology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Chemistry and Pharmacology
    Notes: To estimate the feasibility of isoelectric focusing in a continuous mode, the conditions for obtaining stable and linear pH gradients were first investigated, using a mixture of carrier ampholytes. Then the operating parameters allowing the isoelectric focusing of bovine serum albumin as model protein were determined. A theoretical approach was used to find conditions minimizing the electrohydrodynamic effect, mainly responsible for protein dispersion, for the separation of bovine serum albumin and α-lactalbumin from bovine milk.
    Additional Material: 6 Ill.
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  • 7
    Publication Date: 2019-07-10
    Description: The outstanding problem for useful applications of electrodynamic tethers is obtaining sufficient electron current from the ionospheric plasma. Bare tether collectors, in which the conducting tether itself, left uninsulated over kilometers of its length, acts as the collecting anode, promise to attain currents of 10 A or more from reasonably sized systems. Current collection by a bare tether is also relatively insensitive to drops in electron density, which are regularly encountered on each revolution of an orbit. This makes nighttime operation feasible. We show how the bare tether's high efficiency of current collection and ability to adjust to density variations follow from the orbital motion limited collection law of thin cylinders. We consider both upwardly deployed (power generation mode) and downwardly deployed (reboost mode) tethers, and present results that indicate how bare tether systems would perform as their magnetic and plasma environment varies in low earth orbit.
    Keywords: Spacecraft Design, Testing and Performance
    Type: Tether Technology Interchange Meeting; 379-398; NASA/CP-1998-206900
    Format: text
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  • 8
    Publication Date: 2019-07-13
    Description: Relatively short electrodynamic tethers can use solar power to 'push' against a planetary magnetic field to achieve propulsion without the expenditure of propellant. The groundwork has been laid for this type of propulsion. Important recent milestones include retrieval of a tether in space (TSS-1, 1992), successful deployment of a 20-km-long tether in space (SEDS-1, 1993), and operation of an electrodynamic tether with tether current driven in both directions (PMG, 1993). The planned Propulsive Small Expendable Deployer System (ProSEDS) experiment will use the flight-proven Small Expendable Deployer System (SEDS) to deploy a 5 km bare copper tether from a Delta II upper stage to achieve approximately 0.4 N drag thrust, thus deorbiting the stage. The experiment will use a predominantly 'bare' tether for current collection in lieu of the endmass collector and insulated tether approach used on previous missions. The flight experiment is a precursor to utilization of the technology on the International Space Station for reboost and the electrodynamic tether upper stage demonstration mission which will be capable of orbit raising, lowering and inclination changes, all using electrodynamic thrust. In addition, the use of this type of propulsion may be attractive for future missions at Jupiter.
    Keywords: Spacecraft Design, Testing and Performance
    Type: Propulsion; Jul 13, 1998 - Jul 16, 1998; Cleveland, OH; United States
    Format: application/pdf
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  • 9
    Publication Date: 2019-07-17
    Description: Relatively short electrodynamic tethers can use solar power to 'push' against a planetary magnetic field to achieve propulsion without the expenditure of propellant. The groundwork has been laid for this type of propulsion. NASA began developing tether technology for space applications in the 1960's. Important recent milestones include retrieval of a tether in space (TSS-1, 1992), successful deployment of a 20-km-long tether in space (SEDS-1, 1993), and operation of an electrodynamic tether with tether current driven in both directions-power and thrust modes (PMG, 1993). The planned Propulsive Small Expendable Deployer System (ProSEDS) experiment will demonstrate electrodynamic tether thrust during its flight in early 2000. ProSEDS will use the flight-proven Small Expendable Deployer System (SEDS) to deploy a 5 km bare copper tether from a Delta II upper stage to achieve approximately 0.4 N drag thrust, thus deorbiting the stage. The experiment will use a predominantly 'bare' tether for current collection in lieu of the endmass collector and insulated tether approach used on previous missions. Theory and ground-based plasma chamber testing indicate that the bare tether is a highly-efficient current collector. The flight experiment is a precursor to utilization of the technology on the International Space Station for reboost application and the more ambitious electrodynamic tether upper stage demonstration mission which will be capable of orbit raising, lowering and inclination changes - all using electrodynamic thrust. In addition, the use of this type of propulsion may be attractive for future missions at Jupiter and any other planetary body with a magnetosphere.
    Keywords: Spacecraft Design, Testing and Performance
    Type: Aerospace Sciences; Jan 12, 1998 - Jan 15, 1998; Reno, NV; United States
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