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Chemical Interactions Studies Titles


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Titles:

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Snyder, A., Banks, B., Miller, S., Stueber, T., and Sechkar, E., “Modeling of Transmittance Degradation Caused by Optical Surface Contamination by Atomic Oxygen Reaction With Adsorbed Silicones,” prepared for the 45th Annual International Symposium on Optical Science and Technology Meeting, San Diego, California, June 2001.
 
A numerical procedure is presented to calculate transmittance degradation caused by contaminant films on spacecraft surfaces produced though the interaction of orbital atomic oxygen (AO) with volatile silicones and hydrocarbons from spacecraft component. In the model, contaminant accretion is dependent on the adsorption of species, depletion reactions due to gas-surface collisions, desorption, and surface reactions between AO and silicone producing SiOx (where x is near 2). A detailed description of the procedure used to calculate the constituents of the contaminant layer is presented, including the equations that govern the evolution of fractional coverage by specie type. As an illustrative example of film growth, calculation results using a prototype code that calculates the evolution of surface coverage by specie type is presented and discussed. An example of the transmittance degradation caused by surface interaction of AO with deposited contaminant is presented for the case of exponentially decaying contaminant flux. These examples are performed using hypothetical values for the process parameters.

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Jaworske, D. A., “Hall Effect Thruster Plume Contamination and Erosion Study,” NASA TM-2000-210204, June 2000.

The objective of the Hall effect thruster plume contamination and erosion study was to evaluate the impact of a xenon ion plume on various samples placed in the vicinity of a Hall effect thruster for a continuous 100 hour exposure. NASA Glenn Research Center was responsible for the pre- and post-test evaluation of three sample types placed around the thruster:  solar cell cover glass, RTV silicone, and Kapton®. Mass and profilometry were used to identify the degree of deposition and/or erosion on the solar cell cover glass, RTV silicone, and Kapton® samples. Transmittance, reflectance, solar absorptance, and room temperature emittance were used to identify the degree of performance degradation of the solar cell cover glass samples alone. Auger spectroscopy was used to identify the chemical constituents found on the surface of the exposed solar cell cover glass samples. Chemical analysis indicated some boron nitride contamination on the samples, from boron nitride insulators used in the body of the thruster. However, erosion outweighed contamination. All samples exhibited some degree of erosion, with ±90° positions. For the solar cell cover glass samples, erosion progressed through the antireflective coating and into the microsheet glass itself. Erosion occurred in the solar cell cover glass, TRV silicone, and Kapton® at different rates. All optical properties changed with the degree of erosion. The transmittance of some samples decreased while the reflectance of some samples increased and others decreased. All results are consistent with an energetic plume of xenon ions serving as a source for erosion.

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Illingsworth, M. L., Banks, B. A., Smith, J. W., Jayne, D., Garlick, R. G., Rutledge, S. K., and de Groh, K. K., "Plasma and Beam Facility Atomic Oxygen Erosion of a Transition Metal Complex", Plasma Chemistry and Plasma Processing, Vol. 16, No. 1, 1996.

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Hepp, A. F. and Gaier, J. R., "Reaction of YBa2Cu3O7-d with Gold, Silver, Bismuth, and Lead: Substitution Chemistry and Composite Fabrication", Materials Science Forum, Vol. 137-9, Transtech Publications Ltd., Switzerland, pp.377-94, 1993.

The reaction of YBa2Cu3O7-d with Au, Ag, Bi, and Pb ions or metal is described. Three types of materials were produced: a well-defined series of homogeneous superconductors was obtained for Au ion substitution with little effect on Tc; attempted Ag and Bi ion substitution resulted in multi-phase samples with slightly enhanced Tc; finally, attempts to produce superconducting metal/superconducting ceramics composites with Pb and Bi powders resulted in multi-phase samples with drastically diminished superconducting properties. For Au-substituted superconductors, YBa2(Cu1-xAux)3O7-d , a substitution series (x= 0-0.1) has been synthesized. For x=0.1 there was no change in the a and b lattice parameters (a=3.826 Ĺ and b=3.889 Ĺ) but a 0.06 Ĺ c axis expansion to 11.75 Ĺ was observed. The valence of Cu and Au in YBa2Au3Cu2.7O7-d was investigated using x-ray absorption near-edge structure (XANES). X-ray studies indicate that Au goes into the Cu(1) site and Cu K edge XANES shows that this has little effect on the oxidation state of the remaining copper. A small effect on Tc is observed (Tc=89 for x=0.10). Ag and Bi addition results in a rise in Tc and a decrease in D Tc at low levels (x=0.10 Ag, Tc=94K and D Tc=0.5K; x= 0.02 Bi, Tc=94K and D Tc=1K) relative to typical values for YBa2Cu3O7-d (Tc=91K, D Tc=2K). Attempts at fabrication of Pb- and Pb1-xBix-superconductor composites are described. Cold pressing followed by low temperature (200° C) sintering resulted in a composite which excluded flux below 90K but did not show zero electrical resistance until the metal (alloy) superconducting transition. X-ray diffraction showed the presence of perovskite and metal. Processing at moderate (450° C) or high (950° C) temperatures resulted in oxygen-depleted perovskite and/or metal oxides. These materials displayed greatly degraded superconducting properties. Processing at 800° C resulted in high Tc only for composites containing 90% weight fraction ceramic. Reaction of metal with YBa2Cu3O7-d formed superconducting lead/bismuth-based oxides and other binary oxides.

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Jaworske, D. A. and Jain, S., "Chemical Interactions Between Candidate Radiator Materials and Simulated Lunar Basalt Temperatures up to 1272 K", prepared for the 10th Symposium on Space Nuclear Power, pp.683-88, Albuquerque, New Mexico, January, 1993.

The reactivity of various metal substrates with simulated lunar basalt was studied by mass balance. Candidate materials were submerged in simulated lunar basalt powder and heated to temperatures in excess of 1273 K. After exposure, energy dispersive x-ray analysis was used to provide supporting evidence of the elemental composition of the metal substrates. Niobium, niobium-1%zirconium, and UDIMET 720 gained weight as a result of the high temperature exposure to the basalt and energy dispersive x-ray analysis revealed the presence of iron in these substrates, suggesting that iron diffused from the basalt to the metal substrate. In addition, the basalt lost weight as a result of the high temperature exposure, suggesting the evolution of a volatile species. Other substrates, such as molybdenum and carbon showed no change in weight as a result of the high temperature exposure to the basalt. The results of the high temperature testing using the simulated lunar basalt will be discussed.

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Gaier, James R., Hepp, Aloysius F., Curtis, Henry B., Schupp, Donald A., Hambourger, Paul D., and Blue, James W., “Stability of Bulk Ba2YCu3O(7-x) in a Variety of Environments”, NASA-TM 101401, Prepared for the Fall Meeting of the Materials Research Society, Boston, MA, November 28 – December 2, 1988

Small bars of ceramic Ba2YCu3O(7-x) were fabricated and subjected to environments similar to those that might be encountered during some NASA missions. These conditions include ambient conditions, high humidity, vacuum, and high fluences of electrons and protons. The normal state resistivity or critical current density (J sub c) were monitored during these tests to assess the stability of the material. When normal state resistivity is used as a criterion, the ambient stability of these samples was relatively good, exhibiting only a 2 percent degradation over a 3 month period. The humidity stability was shown to be very poor, and to be a steep function of temperature. Samples stored at 50 C for 40 min increased in normal state resistivity by four orders of magnitude. Kinetic analysis indicates that the degradation reaction is second order with water vapor concentration. It is suspected that humidity degradation also accounts for the ambient instability. The samples were stable to vacuum over a period of at least 3 months. Degradation of J sub c in a 1 MeV electron fluence of 9.7 x 10 to the 14th e(-)/sq cm was determined to be no more than about 2 percent. Degradation of J sub c in a 8.7 x 10 to the 14th p(+)/sq cm of 42 MeV protons was found to be grain size dependent. Samples with smaller grain size and initial J sub c of about 240 A/sq cm showed no degradation, while that with larger grain size and an initial J sub c of about 30 A/sq cm degraded to 37 percent of its original value.


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