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SOLAR WIND SPUTTERING OF LUNAR SOIL ANALOGS: THE EFFECT OF IONIC CHARGE AND MASS H. Hijazi 1 , M. E. Bannister 1 , H. M. Meyer III 2 , C.M. Rouleau 3 , A. F. Barghouty 4 , D.L. Rickman 4 , and F. W. Meyer 1 1 Physics Division, Oak Ridge National Laboratory, Oak Ridge, TN 37831-6372 USA, 2 Materials Science and Technology Division, Oak Ridge National Laboratory, Oak Ridge, TN 37831-6064 USA, 3 Center for Nanophase Materials Sciences, Oak Ridge National Laboratory, Oak Ridge, TN 37831-6488, 4 MSFC, Huntsville, AL 35805 Multicharged Ion Research Facility (MIRF) 45 th Lunar and Planetary Science Conference The Woodlands, TX, March 18 – 22, 2014 E-mail: [email protected] Acknowledgements : Research sponsored by NASA grant 10-LASER10-0053, by the LDRD program of Oak Ridge National Laboratory, managed by UT-Battelle, LLC, for the U.S. Department of Energy, and performed in part via the ORNL SHaRE User program and at the Center for Nanophase Materials Sciences user facility, which is sponsored at Oak Ridge National Laboratory by the Scientific User Facilities (SUF) Division, U.S. Department of Energy. Solar wind sputtering of lunar regolith induces compositional changes in the lunar surface and contributes to its erosion rate, and affects the composition of lunar exosphere. Solar wind-lunar surface interactions may further play a role in the accumulation of hydrogen and water on the moon’s surface. Our goal in the present work is to assess the sputtering contribution of the highly charged, heavy minority solar wind constituents in anorthite, a lunar highlands soil analog. Total absolute sputtering yields are determined using a sensitive quartz microbalance by measuring the thickness change of a thin anorthite film deposited on a gold coa- ted quartz sensor induced by a known fluence of a well- characterized, solar wind relevant ion beam. Characteristics of lunar surface and the solar wind >90% of solar wind consists of protons; but it also contains heavier constituents in high charge states Lunar exosphere pressure ~ 10 -11 Torr No SWHI exosphere collisions prior to impact: unchanged incident charge state and velocity No sputtering product collisions in exosphere: sputtered particles with v > lunar escape velocity leave exosphere sputtered particles with v < lunar return to lunar surface All solar wind particles have same average velocity , which can vary between ~0.3 - 1 keV/amu For insulator targets only: Resonance neutralization (I), causes ejection of a neutralized, non-thermal lattice anion (i.e. O atom in the case of a metal oxide). Auger neutralization (II) produces a self-trapped exciton (STE) that decays into an F-center and H-center in the case of alkali halide targets, or E’ centers in the case of SiO 2 . Physical Sputtering Heavier 1+ ions have a higher physical sputtering yield than iso-velocity protons due to more efficient energy transfer: yield for Ar + ~100 x larger than that for H + Solar wind velocity Potential sputtering Metal oxides can have different types of potential sputtering, each having unique kinetic energy, charge state, and saturation dependence defect mediated desorption kinetically assisted potential sputtering Difficult to predict which dominates for those oxides not yet studied; no previous measurements at solar wind relevant velocities need to use suitable analog material or actual lunar regolith sample Solar wind velocity Fundamental Mechanisms Motivation and Goal Approach Apparatus Quartz Microbalance Method Ar 6+ on Au Ar 6+ on anorthite Check of independently absolute calibration stoichiometry Al/Ca Si/Ca Bulk 2.4 2.2 Evaporation 2.7 0.2 PLD 2.1 1.9 XPS anorthite (CaAl 2 Si 2 O 8 ) film stoichiometry analysis Pulsed Laser Deposition yields coating with stoichiometry that is consistent with chemical formula Vapor deposition using EFM-3 yields coating with poor stoichiometry Ion neutralization potential energy (eV) Yield Experiment Yield SRIM Total sputtering yield enhancement Ar q+ /Ar + H + 13.6 0.0038 ±0.0008 0.0042 Ar 1+ 16.00 0.30±0.06 0.251 1 Ar 2+ 48.34 0.33±0.07 1.1 4+ 162.04 0.35±0.06 1.17 6+ 341.6 0.38±0.07 1.27 7+ 474.8 0.42±0.07 1.4 8+ 627.6 0.44±0.06 1.47 Ar 9+ 1023.7 0.50±0.07 1.67 Quartz crystal microbalane (QCM) measurements Total absolute sputtering yields for anorthite thin film at 500 eV/amu H + , Ar + measured sputtering yields in excellent agreement with TRIM Ar 9+ sputtering yield >130 times greater than that for same velocity protons Ar q+ induced sputtering of anorthite shows significant charge state dependence - evidence of potential sputtering mechanism Total absolute sputtering yields for gold thin film at 500 eV/amu Ar charge State Yield 2+ 9.0±1.8 3+ 9.1±1.8 4+ 8.0 ±1.6 8+ 8.7±1.74 9+ 8.0±1.6 No charge state dependence of sputtering yields – absence of potential sputtering mechanism Element 20 keV 20 keV O enhanced O 2.24 6.72 Ca 0.3539 0.3539 Al 0.3858 0.3858 Si 0.3307 0.3307 Total yield 0.2506 0.523 Quadrupole mass spectrometry (QMS) measurements For anorthite, enhancement of O, H 3 O + mass peaks evident for Ar 9+ compared to Ar 2+ - by average factor of about 3 For impact on Ta flag, no significant enhancement of O, OH, H 2 O, H 3 O + Background subtracted mass spectra for Ar 9+ and Ar 2+ ions incident on Ta and anorthite Effect of factor 3 greater O sputtering on total anorthite sputtering yield by Ar 9+ TRIM TRIM plus potential Observed total yield enhancement is consistent with assumption that, for an anorthite target, only O sputtering is enhanced for incident multi- charged vs. singly charged ions, by a factor determined by QMS. Y potential = Y q+ - Y + With above power law fit of Ar q+ potential sputtering, TRIM and QMS result, can estimate sputtering yields for all charge states of all solar wind ions Summary: As a result of the combined effects of higher physical sputtering yields due to their greater mass and the presence of potential sputtering enhancement due to their high charge states, total yields of the minority solar wind constituent ions can exceed those for same velocity protons by factors much greater than 100 Quadrupole mass spectrometry measurements indicate that the dominant effect of potential sputtering of lunar soil analogs at solar wind relevant energies and charge states is a significant enhancement of oxygen emission. Excellent quantitative agreement with QCM result Isolation and parameterization of potential sputtering Anorthite thin film production Using a sensitive quartz microbalance, independently absolute sputtering yields have been measured for 500 eV/amu H + , and Ar q+ (q=1-9) ions incident on Au and anorthite Y = D A x A x f / N inc D A = 12.4 ng/cm 2 s /(1 / 2 ) A - beam area; a - sensor sensitivity form factor = 1.031 mm Aluminum Ta flag

SOLAR WIND SPUTTERING OF LUNAR SOIL ANALOGS: THE … · 9+ 1023.7 . 0.50±0.07 : 1.67 . Quartz crystal microbalane (QCM) measurements Total absolute sputtering yields for anorthite

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Page 1: SOLAR WIND SPUTTERING OF LUNAR SOIL ANALOGS: THE … · 9+ 1023.7 . 0.50±0.07 : 1.67 . Quartz crystal microbalane (QCM) measurements Total absolute sputtering yields for anorthite

SOLAR WIND SPUTTERING OF LUNAR SOIL ANALOGS: THE EFFECT OF IONIC CHARGE AND MASS H. Hijazi1, M. E. Bannister1, H. M. Meyer III2, C.M. Rouleau3, A. F. Barghouty4, D.L. Rickman4, and F. W. Meyer1 1Physics Division, Oak Ridge National Laboratory, Oak Ridge, TN 37831-6372 USA, 2Materials Science and

Technology Division, Oak Ridge National Laboratory, Oak Ridge, TN 37831-6064 USA, 3Center for Nanophase Materials Sciences, Oak Ridge National Laboratory, Oak Ridge, TN 37831-6488, 4MSFC, Huntsville, AL 35805

Multicharged Ion Research

Facility (MIRF)

45th Lunar and Planetary Science Conference The Woodlands, TX, March 18 – 22, 2014 E-mail: [email protected]

Acknowledgements : Research sponsored by NASA grant 10-LASER10-0053, by the LDRD program of Oak Ridge National Laboratory, managed by UT-Battelle, LLC, for the U.S. Department of Energy, and performed in part via the ORNL SHaRE User program and at the Center for Nanophase Materials Sciences user facility, which is sponsored at Oak Ridge National Laboratory by the Scientific User Facilities (SUF) Division, U.S. Department of Energy.

Solar wind sputtering of lunar regolith induces compositional changes in the lunar surface and contributes to its erosion rate, and affects the composition of lunar exosphere. Solar wind-lunar surface interactions may further play a role in the accumulation of hydrogen and water on the moon’s surface. Our goal in the present work is to assess the sputtering contribution of the highly charged, heavy minority solar wind constituents in anorthite, a lunar highlands soil analog.

Total absolute sputtering yields are determined using a sensitive quartz microbalance by measuring the thickness change of a thin anorthite film deposited on a gold coa-ted quartz sensor induced by a known fluence of a well- characterized, solar wind relevant ion beam.

Characteristics of lunar surface and the solar wind >90% of solar wind consists of protons; but it also contains heavier constituents in high charge states

Lunar exosphere pressure ~ 10-11 Torr • No SWHI exosphere collisions prior to impact:

unchanged incident charge state and velocity

• No sputtering product collisions in exosphere: sputtered particles with v > lunar escape velocity leave exosphere

sputtered particles with v < lunar return to lunar surface • All solar wind particles have same average

velocity , which can vary between ~0.3 - 1 keV/amu

For insulator targets only: Resonance neutralization (I), causes ejection of a neutralized, non-thermal lattice anion (i.e. O atom in the case of a metal oxide). Auger neutralization (II) produces a self-trapped exciton (STE) that decays into an F-center and H-center in the case of alkali halide targets, or E’ centers in the case of SiO2.

Physical Sputtering

Heavier 1+ ions have a higher physical sputtering yield than iso-velocity protons due to more efficient energy transfer: yield for Ar+ ~100 x larger than that for H+

Solar wind velocity

Potential sputtering

Metal oxides can have different types of potential sputtering, each having unique kinetic energy, charge state, and saturation dependence • defect mediated desorption • kinetically assisted potential sputtering

Difficult to predict which dominates for those oxides not yet studied; no previous measurements at solar wind relevant velocities

• need to use suitable analog material or actual lunar regolith sample

Solar wind velocity

Fundamental Mechanisms Motivation and Goal

Approach

Apparatus

Quartz Microbalance Method

Ar6+ on Au Ar6+ on anorthite

Check of independently absolute calibration

stoichiometry Al/Ca Si/Ca

Bulk 2.4 2.2

Evaporation 2.7 0.2

PLD 2.1 1.9

XPS anorthite (CaAl2Si2O8) film stoichiometry analysis

Pulsed Laser Deposition yields coating with stoichiometry that is consistent with chemical formula

Vapor deposition using EFM-3 yields coating with poor stoichiometry

Ion neutralization potential

energy (eV)

Yield Experiment

Yield SRIM

Total sputtering yield

enhancement Arq+/Ar+

H+ 13.6 0.0038 ±0.0008

0.0042

Ar1+ 16.00 0.30±0.06 0.251 1 Ar2+ 48.34 0.33±0.07 1.1 4+ 162.04 0.35±0.06 1.17 6+ 341.6 0.38±0.07 1.27 7+ 474.8 0.42±0.07 1.4 8+ 627.6 0.44±0.06 1.47

Ar9+ 1023.7 0.50±0.07 1.67

Quartz crystal microbalane (QCM) measurements Total absolute sputtering yields for anorthite thin film at 500 eV/amu

• H+, Ar+ measured sputtering yields in excellent agreement with TRIM • Ar9+ sputtering yield >130 times greater than that for same velocity protons • Arq+ induced sputtering of anorthite shows significant charge state dependence - evidence of potential sputtering mechanism

Total absolute sputtering yields for gold thin film at 500 eV/amu

Ar charge State Yield

2+ 9.0±1.8

3+ 9.1±1.8

4+ 8.0 ±1.6

8+ 8.7±1.74

9+ 8.0±1.6

No charge state dependence of sputtering yields – absence of potential sputtering mechanism

Element 20 keV 20 keV O enhanced

O 2.24 6.72 Ca 0.3539 0.3539 Al 0.3858 0.3858 Si 0.3307 0.3307 Total yield 0.2506 0.523

Quadrupole mass spectrometry (QMS) measurements

For anorthite, enhancement of O, H3O+ mass peaks evident for Ar9+ compared to Ar2+ - by average factor of about 3

For impact on Ta flag, no significant enhancement of O, OH, H2O, H3O+

Background subtracted mass spectra for Ar9+ and Ar2+ ions incident on Ta and anorthite

Effect of factor 3 greater O sputtering on total anorthite sputtering yield by Ar9+

TRIM TRIM plus potential

Observed total yield enhancement is consistent with assumption that, for an anorthite target, only O sputtering is enhanced for incident multi-

charged vs. singly charged ions, by a factor determined by QMS.

Ypotential = Yq+ - Y+

With above power law fit of Arq+ potential sputtering, TRIM and QMS result, can estimate sputtering yields for all charge states of all solar wind ions

Summary:

As a result of the combined effects of higher physical sputtering yields due to their greater mass and the presence of potential sputtering enhancement due to their high charge states, total yields of the minority solar wind constituent ions can exceed those for same velocity protons by factors much greater than 100

Quadrupole mass spectrometry measurements indicate that the dominant effect of potential sputtering of lunar soil analogs at solar wind relevant energies and charge states is a significant enhancement of oxygen emission.

Excellent quantitative agreement with QCM result

Isolation and parameterization of potential sputtering

Anorthite thin film production

Using a sensitive quartz microbalance, independently absolute sputtering yields have been measured for 500 eV/amu H+, and Arq+ (q=1-9) ions incident on Au and anorthite

Y = DA x A x ∆f / Ninc DA = 12.4 ng/cm2s /(1 − 𝑒−𝐴/𝜋𝑎2) A - beam area; a - sensor sensitivity form factor = 1.031 mm

Aluminum

Ta flag