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  • Other Sources  (38)
  • 2005-2009  (1)
  • 2000-2004  (4)
  • 1990-1994  (11)
  • 1965-1969  (19)
  • 1950-1954  (3)
  • 1
    Publication Date: 2011-08-11
    Description: Plasma energy density, conductivity and temperature measurements at various pressures
    Keywords: PHYSICS, PLASMA
    Type: JOURNAL OF APPLIED PHYSICS
    Format: text
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  • 2
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    In:  Other Sources
    Publication Date: 2011-08-11
    Description: Measurement of plasma density generated by underwater explosions, noting modes of electrical discharge and shock front role
    Keywords: PHYSICS, PLASMA
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  • 3
    Publication Date: 2016-06-07
    Keywords: GENERAL
    Type: Conf. on Hypersonic Aircraft Technol.; p 527-540
    Format: text
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  • 4
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    Publication Date: 2019-05-30
    Description: Data from ground photography of Mars covering portions of Mariner IV path, noting position of oases and canals
    Keywords: SPACE SCIENCES
    Type: ICARUS
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  • 5
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    Publication Date: 2019-06-28
    Description: Orbital debris issues associated with maintaining a Space Shuttle External Tank (ET) on orbit are presented. The first issue is to ensure that the ET does not become a danger to other spacecraft by generating space debris, and the second is to protect the pressurized ET from penetration by space debris or meteoroids. Tests on shield designs for penetration resistance showed that when utilized with an adequate bumper, thermal protection system foam on the ET is effective in preventing penetration.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 92-1411
    Format: text
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  • 6
    Publication Date: 2019-05-30
    Description: Plasma energy density and conductivity measured at pressures from 3 to 120 kilobars
    Keywords: PHYSICS, PLASMA
    Type: NASA-CR-78481
    Format: application/pdf
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  • 7
    Publication Date: 2019-05-24
    Description: Mars surface as seen by Mariner IV photographs
    Keywords: SPACE SCIENCES
    Type: NASA-CR-64466 , TN-701-66-10
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  • 8
    Publication Date: 2019-06-28
    Description: This report summarizes the damage analyses performed on the tether cable used for the tethered satellite system (TSS), for the damage that could be caused by meteoroid or orbital debris impacts. The TSS consists of a tethered satellite deployer and a tethered satellite. The analytical studies were performed at Marshall Space Flight Center (MSFC) with the results from the following tests: (1) hypervelocity impact tests to determine the 'critical' meteoroid particle diameter, i.e., the maximum size of a meteoroid particle which can impact the tether cable without causing 'failure'; (2) electrical resistance tests on the damaged and undamaged tether cable to determine if degradation of current flow occurred through the damaged tether cables; and (3) tensile load tests to verify the load carrying capability of the damaged tether cables. Finally, the HULL hydrodynamic computer code was used to simulate the hypervelocity impact of the tether cable by particles at velocities higher than can be tested, to determine the extent of the expected tether damage.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-TM-108404 , NAS 1.15:108404
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  • 9
    Publication Date: 2019-06-28
    Description: The effect of acoustic coupling on random and harmonic plate vibrations is studied using two numerical models. In the coupled model, the plate response is obtained by integration of the nonlinear plate equation coupled with the nonlinear Euler equations for the surrounding acoustic fluid. In the uncoupled model, the nonlinear plate equation with an equivalent linear viscous damping term is integrated to obtain the response of the plate subject to the same excitation field. For a low-level, narrow-band excitation, the two models predict the same plate response spectra. As the excitation level is increased, the response power spectrum predicted by the uncoupled model becomes broader and more shifted towards the high frequencies than that obtained by the coupled model. In addition, the difference in response between the coupled and uncoupled models at high frequencies becomes larger. When a high intensity harmonic excitation is used, causing a nonlinear plate response, both models predict the same frequency content of the response. However, the level of the harmonics and subharmonics are higher for the uncoupled model. Comparisons to earlier experimental and numerical results show that acoustic coupling has a significant effect on the plate response at high excitation levels. Its absence in previous models may explain the discrepancy between predicted and measured responses.
    Keywords: ACOUSTICS
    Type: NASA-TM-107740 , NAS 1.15:107740
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  • 10
    Publication Date: 2019-06-28
    Description: Mixtures of pure liquid hydrocarbons are capable of foaming. Nine hydrocarbons were mixed in pairs, in all possible combinations, and four proportions of each combination. These mixtures were sealed in glass tubes, and the foaming was tested by shaking. Mixtures of aliphatic with other aliphatic hydrocarbons, or of alkyl benzenes with other alkyl benzenes, did not foam. Mixtures of aliphatic hydrocarbons with alkyl benzenes did foam. The proportions of the mixtures greatly affected the foaming, the maximum foaming of 12 of 20 pairs being at the composition 20 percent aliphatic hydrocarbon, 80 percent alkyl benzene. Six seconds was the maximum foam lifetime of any of these mixtures. Aeroshell 120 lubricating oil was fractionated into 52 fractions and a residue by extraction with acetone in a fractionating extractor. The index of refraction, foam lifetime, color, and viscosity of these fractions were measured. Low viscosity and high index fractions were extracted first. The viscosity of the fractions extracted rose and the index decreased as fractionation proceeded. Foam lifetimes and color were lowest in the middle fractions. Significance is attached to the observation that none of the foam lifetimes of the fractions or residue is as high as the foam lifetime of the original Aeroshell, indicating that the foaming is not due to a particular foaming constituent, but rather to the entire mixture.
    Keywords: Inorganic, Organic and Physical Chemistry
    Type: NACA-TN-2032 , AD-A801543
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