laboratory studies of lunar dust...
TRANSCRIPT
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Laboratory Studies of Lunar Dust Transport
X. Wang, M. Horanyi and S. Robertson
Colorado Center for Lunar Dust and Atmospheric Studies (CCLDAS)
4.15.2010
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Lunar plasma Environment
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Image of Surveyor 6 lunar lander showing a glow on the western lunar horizon after sunset.
Evidence of electrostatic dust transport on the lunar surface
Zodiacal light
Horizon glow
The “Horizon Glow” is due to light scattered from dust particles near the lunar surface.
Dust grains with radius of 5-6 µm at about 10-30cm from the surface.
Horizon glow ~107 too bright to be explained by micro-meteoroid generated ejecta.
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Dust release from the lunar surface
Sketches drawn by Apollo 17 astronauts of sunrise as viewed from lunar orbit
The linear streamers are attributed to dust particles (0.1µm scale) leaving the lunar surface.
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Lunar Ejecta and Meteorites (LEAM) Experiment
The LEAM was deployed during the Apollo 17 mission
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Lower velocity impacts instead of hypervelocity impacts were detected near terminators, which are attributed to electrostatic dust transport.
Dust detections from the LEAM experiment
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Photoelectric Charging on the Lunar Surface
UV Radiation
• Differential photoelectric charging near the boundary between lit and shadowed region.
• It has been suggested that time dependent charging at the terminator region may lead to ‘super-charging’, and the lift-off of lunar fines [Criswell and De, 1977].
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UV Source
Light Stopper
Quartz Lens
To Pumps To High Impedance Circuit
Zirconium surfaces
Zirconium surface arrangement
Top view of light stopper
Laboratory Setup
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Surpercharging near Moving Lit-Dark Boundaries
Surface L 0 1 2 3 4 5
Shadow
UV light
Surface L is ‘supercharged’ when the shadow approaches it (i.e. the progression of sunset).
* X. Wang, M. Horanyi, Z. Sternovsky, S. Robertson and G. E. Morfill, GRL., 34, L16104 (2007).
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e
e Surface
UV light
e e Surface
e Surface
This is because the newly darken surface attracts more electrons from still lit surfaces but without emitting its own.
Surpercharging near Moving Lit-Dark Boundaries
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We expect the largest increase in the potential due to ’supercharging’ when the charging time of a surface is similar to the transition time of the shadow.
Potential on surface L when the shadow moves at various speeds
Surpercharging near Moving Lit-Dark Boundaries
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Dust Levitation in Plasma Sheath
JSC-1 lunar simulants (< 25 µm) levitate at 1.1 cm above the surface (Sickafoose et al., 2002a).
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Dust Levitation in Plasma Sheath
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Dust Levitation in Plasma Sheath
Plasma
Sheath
Surface
Presheath
_E force
Gravity
Dust levitates when Fe – Fg = 0
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Dust transport experiments
CCD camera
Emissive probe
Filaments
Dust pile
Graphite plate
Vacuum pump
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Dust transport movie (JSC Mars simulant)
< 25 µm
~100 µm
< 25 µm
~ 100 µm
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Dust Ring
Bull’s Eye Pattern
Initial Pile
Uniform Spreading
Image of initial dust pile on the surface (0 min) and images of dust spreading on the surface at 1 min, 20 min and 45 min after exposure to the plasma.
Dust Transport Still Images
* X. Wang, M. Horányi and S. Robertson, JGR, 114, A05103 (2009).
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qE qE
Radial potential scans 2 mm above the dust pile sitting on the graphite surface
• Dust particles charge positively because negative bias on the plate collects ions.
• Electric field points outward to push dust spread on the surface.
• The potential profiles also indicate ‘bull’s eye’ and ‘ring’ patterns.
Horizontal Electrostatic Force
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Dust deposits on the side wall and top of an adjacent insulating block, which indicates a dust hopping motion.
Dust Lift-off Observations
CCLDAS
Insulator
6 mm
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qE
• A non-monotonic potential structure, a potential dip, is found above an insulating disc when the sheath thickness (~3cm) is larger than the radius of the disc.
• Electric field near the insulating disc points upward and increases with the plate bias voltage, which causes the dust lift-off.
Vertical potential scans above an insulating disc (d = 1.1cm) sitting on the graphite surface
Vertical electrostatic force
CCLDAS
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Potential built-up above the dust pile
• The sheath thickness is larger than the radius of the disc.
• A negative potential barrier in the sheath returns most electrons and accelerate ions toward the dust pile.
• Dust particles collect more ions to charge positively and build a positive potential barrier that tends to equalize the electron and ion fluxes.
The graphite surface is biased at -80V and diameter of the disc is 0.7cm.
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• Dsheath = 2.6 cm and Rdisc= 2.2cm.
• Qedge ≈ 3Qcenter.
• Combined with electric field distributions, a threshold could be created at a position where QE moves outer dust particles but not the central dust particles, which results in a ‘bull’s eye’ formation.
Radial charge distribution during the spread
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• Charge on dust on the central disc increases when the surrounding ring expands
• Electric field is re-established when the graphite surface is exposed to the plasma again.
• Thus, central particles restart to spread and form a single ‘ring’ at the end.
Charge on central dust vs. ring expansion
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Dust transport in plasma with an electron beam
Emissive probe
Filament
Dust patch
Graphite plate
Vacuum pumps
Electron beam source
CCD camera
Liners Liners
Metal plate
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Electron beam at 35eV
Langmuir probe I-V trace shows an electron beam at 35 eV.
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Bi-Maxwellian electrons
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Currents to the dust and graphite surfaces
Jb is electron beam current density.
Jec is cold electron current density.
Jeh is hot electron current density.
Ji is ion current density and equals
Jse is secondary electron current density and Jse = kJb.
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Potential distributions above the dust surface
Horizontal potential profiles Vertical potential profiles
Matching beam: Jb ≈ Ji
Dust surface
Graphite surface
Graphite surface
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Potential distributions above the dust surface
Surface potential vs. Beam energy Electric field vs. Beam energy
• Secondary electrons are not negligible when beam energy is greater than 50eV.
• Potentials on the dust surface are more negative than on the graphite surface, indicating γSE_dust < γSE_graphite.
• E⊥ is increased in an order of magnitude that significantly increases the dust release rate.
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Strong beam: Jb > Ji
• Potential on both dust and graphite surface follows the beam energy.
• E// is near zero.
• E⊥ has no significant increasement.
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Weak beam: Jb < Ji
• Potentials on both dust and graphite surfaces are independent of the beam energy.
• E// is near zero.
• E⊥ is near constant.
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Dust transport observation (Jb ≈ Ji, Eb=70 eV)
This is more likely to happen on the night-side lunar surface when the Moon enters Earth’s magnetotail and the high energy electron fluxes create the secondary electrons.
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Dust Transport in Craters
The dust pond is most likely formed due to electrostatic dust transport to the bottom of the crater from outside and the upper slope.
(Renno, 2008)
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E Beam source
Shadowed Impacted 1
23 4
5
6
e
e
Electron Beam Induced Potential Differences
Half Tube Plasma
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Impacted
Shadowed
Dust particles on the impacted slope move downhill. Dust particles on the shadowed slope have no transport.
Beam Source Far from The Tube
Impacted
Shadowed
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Impacted
Shadowed
Impacted
Shadowed
Beam Source near The Tube
Dust hopping process goes faster than surface transport.
Impacted
Shadowed
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Summary
• ‘Supercharging’ effect has been shown with moving lit/dark boundaries, which increases possibilities of dust lift-off near lunar terminators.
• Dust levitation in plasma sheath has been shown.
• Dust has been observed to transport on a surface that repels most of electrons and collects ions in plasma.
• Also, dust transports on a surface in plasma with an electron beam due to the secondary electrons emitting from surfaces. This is more likely to happen on the night-side lunar surface.
• Dust transport in craters is under investigation in laboratory.
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Potential in situ measurements on lunar surface
Double probe for characterizing photoelectrons
* X. Wang, M. Horányi and S. Robertson, JGR, 113, A08108 (2008).
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Potential in situ measurements on lunar surface
Langmuir Probes for the Lunar Surface (LPLUS)
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Thank You