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  • PHYSICS, ATOMIC, MOLECULAR, AND NUCLEAR  (4)
  • Spacecraft Propulsion and Power  (2)
  • 2020-2022
  • 2010-2014  (2)
  • 1975-1979
  • 1970-1974  (4)
  • 1920-1924
  • 1905-1909
  • 1
    Publication Date: 2019-06-27
    Description: We have calculated the polarization fraction of the Lyman-alpha radiation emitted in e/-/-H/1s/ collisions using the Glauber, Born, and various Vainshtein approximations, and have compared these predictions with observation. We find that the Born, Glauber and all forms of the Vainshtein yield results which are very close to each other and to the data in the energy range from 30 to 700 eV. The comparatively small differences between the various approximations are detailed in the text; also, the reason for the close agreement of the predicted polarization fractions - although the computed 1s-2p total and differential cross sections are not so close - is explained. With respect to the Glauber approximation, the importance of computing the phase integral along a direction perpendicular to the momentum transfer q at each value of q, is stressed.
    Keywords: PHYSICS, ATOMIC, MOLECULAR, AND NUCLEAR
    Type: Journal of Physics; vol. 5
    Format: text
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  • 2
    Publication Date: 2019-06-27
    Description: Glauber scattering amplitudes for atomic hydrogen excitation by electrons or protons, presenting closed form expressions requiring no numerical integration
    Keywords: PHYSICS, ATOMIC, MOLECULAR, AND NUCLEAR
    Type: ; - ASTRONOMY 1969- TE
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Description: Glauber approximations for elastic and inelastic scattering of protons by ground state hydrogen atoms, comparing with measurements
    Keywords: PHYSICS, ATOMIC, MOLECULAR, AND NUCLEAR
    Type: ; 35 (
    Format: text
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  • 4
    Publication Date: 2019-06-27
    Description: Glauber and Vainshtein approximations for cross sections of 1s-2p excitation during inelastic electron-atomic hydrogen scattering
    Keywords: PHYSICS, ATOMIC, MOLECULAR, AND NUCLEAR
    Type: ; UGREVUE(
    Format: text
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  • 5
    Publication Date: 2019-07-12
    Description: An investigation into the merits of battery powered Electro Hydrostatic Actuation (EHA) for Thrust Vector Control (TVC) of the Ares I and Ares V launch vehicles is described. A top level trade study was conducted to ascertain the technical merits of lithium-ion (Li-ion) and thermal battery performance to determine the preferred choice of an energy storage system chemistry that provides high power discharge capability for a relatively short duration.
    Keywords: Spacecraft Propulsion and Power
    Type: NASA/TM-2011-216899 , E-17478
    Format: application/pdf
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  • 6
    Publication Date: 2019-07-13
    Description: The National Aeronautics and Space Administration is developing battery and fuel cell technology to meet the expected energy storage needs of human exploration systems. Improving battery performance and safety for human missions enhances a number of exploration systems, including un-tethered extravehicular activity suits and transportation systems including landers and rovers. Similarly, improved fuel cell and electrolyzer systems can reduce mass and increase the reliability of electrical power, oxygen, and water generation for crewed vehicles, depots and outposts. To achieve this, NASA is developing non-flow-through proton-exchange-membrane fuel cell stacks, and electrolyzers coupled with low permeability membranes for high pressure operation. The primary advantage of this technology set is the reduction of ancillary parts in the balance-of-plant fewer pumps, separators and related components should result in fewer failure modes and hence a higher probability of achieving very reliable operation, and reduced parasitic power losses enable smaller reactant tanks and therefore systems with lower mass and volume. Key accomplishments over the past year include the fabrication and testing of several robust, small-scale non-flow-through fuel cell stacks that have demonstrated proof-of-concept. NASA is also developing advanced lithium-ion battery cells, targeting cell-level safety and very high specific energy and energy density. Key accomplishments include the development of silicon composite anodes, lithiatedmixed- metal-oxide cathodes, low-flammability electrolytes, and cell-incorporated safety devices that promise to substantially improve battery performance while providing a high level of safety.
    Keywords: Spacecraft Propulsion and Power
    Type: NASA/TM-2011-216964 , AIAA Paper 2010-8709 , E-17569 , Space 2010 Conference and Exposition; Aug 30, 2010 - Sep 02, 2010; Anaheim, CA; United States
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