The Lunar Surface: A Dusty Plasma Laboratory
Transcription
The Lunar Surface: A Dusty Plasma Laboratory
The Lunar Surface: A Dusty Plasma Laboratory M. Horanyi, D. Brain, A. Colette, K. Drake, E. Grün, S. Kempf, T. Munsat, S. Robertson, Z. Sternovsky, X. Wang & CCLDAS Team NASA Lunar Institute: Colorado Center for Lunar Dust and Atmospheric Studies Outline: 1) Dusty Plasmas 2) Outstanding Lunar Issues 3) Laboratory Experiments 4) Space-born Experiment (LDEX) 5) Surface-Experiments Fall AGU 2011 1 Dusty Plasmas e, i1 , i1 , i1 , … and dust+/duste and dust + dust Fall AGU 2011 + and dust 2 Dusty Plasmas New physics: Dust is many orders of magnitude heavier than ions and can carry many orders of magnitude larger + or – time dependent charge. new temporal & spatial scales unusual dynamics new waves & instabilities Dust charge: electron and ion fluxes secondary and photoelectrons dust – dust collisions Fall AGU 2011 3 Unresolved lunar issues Fall AGU 2011 4 CeO2 (Cerium-oxide) experiments UV lamps Single-sided planar Langmuir probe Tantalum Ceramic coating foil Collector Biased grid Langmuir Probe CeO2 Zr surface Fall AGU 2011 5 CeO2 experiments Over CeO2 Over Zr 1.4 1.4 float float 1.2 0V 1.2 -20 V -20 V -40 V Current (mA) 1.0 0.5 0.8 0.4 0.6 Current (µA) Current (mA) 1.0 0.4 0.2 0.0 -40 0V -20 0.3 0.2 0.1 0.0 0 Bias Voltage (V) -0.1 +20 V bias +10 V bias +5 V bias 0 V bias -5 V bias -10 V bias -20 V bias -40 V 0.8 0.6 0.4 0.2 0.0 20 40 -40 (a) -20 0 Bias Voltage (V) 20 40 Derivative (arb. units) 0.06 0.05 0.04 0.03 0.02 0.01 0.00 -0.01 30 Fall AGU 2011 20 10 (b) A. Dove P41C-1635 (Thursday) 6 Motivation Dust Levitation Dusty Sheath Potential Motivation Dust Levitation Dusty Sheath Dusty Plasma Sheath Grain Levitation XXXXXX Colwell et al.: LUNAR REGOLITH AND DUST DYNAMICS Motivation Dust Levitation Dusty Sheath ng the Sheath F< G!248H I< I3J3J342 429 ;< K0#)35 Jamey Szalay Dusty Sheath Simulation Jamey Szalay Dusty Sheath Simulation Arnas et al., 2001 Jamey Szalay Dusty Sheath Simulation 7 L$%3#$ 439%- 2-(R4% &' 54%,# &'34%7 3") )1&# 23-#*'4% &1-,3'% 2(#%"< Fall AGU 2011 0$# &'34%7 >%-&1& #$% 2(&*#*(": 587 ^1&# 23-#*'4% 2(#%"#*34 %"%-09 3 2(#%"#*34 ?%44+ >%-&1& #$% 2(&*#*(": J. Szalay P13D-1708 ;3,< >< L$%3#$ 439%- 2-(R4%& ?*#$(1# 3") ?*#$ )1&# 23-#*'4%&: Q:Q: /01)21345 6!075) 32 1.) 6!)8)2%) 0" 4 9:81 %50:9 D*01-% W 0*>%& #$% 2(#%"#*34 2-(R4%& ?*#$ -%&2%'# #( #$% 7 Plasma interaction with a magnetic dipole field Dipolar Magnetic field (~600 G at the surface) IEA Emissive probe Vacuum pump N S Insulating surface Filament ! Effects of Surface Magnetic Fields Electrons are magnetized (re < d) Ions are un-magnetized (ri > d) Fall AGU 2011 ! 9 Potential contours above the surface along the dipole axis Non-monotonic sheath ! • More positive surface potential than the bulk to reflect the ions back into the plasma. • Potential minimum due to collisions and magnetic-mirror-trapping. Horizontal fluctuations Fall AGU 2011 10 Surface potential and electric field profiles • Fluctuation due to shielding, focusing ! • Highest electric fields at the cusps may enhance the dust transport. ! Xu Wang P43F-06 (Thursday) I II III Fall AGU 2011 IV 11 LADEE: LDEX MCP detector for ions (high sensitivity) and integrated signal E-field Ions e- Incoming dust Hemispherical target Target collects electrons (low sensitivity) Fall AGU 2011 12 Testing and Initial Calibration • Performed at the CCLDAS facility • Velocity range 1–8 km/s LADEE velocity • Size range 0.2 – 1.5 µm • Total number of particles shown • Black: particles detected by LDEX • Red: not detected by LDEX • 65% is detected Velocity [km/s] • Dust flux is reduced by the 3 grids over the aperture (90% open area) and the 90% duty cycle of LDEX • (0.9)4 = 0.656 13 Fall AGU 2011 13 The measurement establishes a direct link of the grains composition to its origin on the surface (compositional mapping). In the course of the mission a dust spectrometer is collecting many thousands of submicron samples from a greater part of the entire surface and determines their origin and composition. It thus combines in situ analysis, which otherwise could only be achieved by a lander, with the much better surface coverage of a remote sensing method. LDEX Expectations Figure 1. Schematics of dust spectrometry of a planetary surface. Ejecta particles lifted by micro-meteoroid impacts from the satellites' surface are analyzed in situ by a sensor in combination with a high-resolution dust mass spectrometer. By tracing back the trajectory to the surface compositional maps of the surface are generated. The analysis of emitted solids is complementary to studies by remote sensing methods (e.g. by infrared spectroscopy) and analysis of the gas phase (by an ion and neutral mass spectrometers). It is important that both, solid and gas phases be measured. For example, Cassini’s dust detector CDA (Srama et al., 2004) found sodium salts in the dust particles from Saturn’s satellite Enceladus (e.g. Postberg et al., 2009), while high-resolution spectroscopy and the Cassini INMS did not detect any sodium in the emerging plume gas or at the moon’s surface (Schneider et al., 2009; Waite et al., 2009). Only the combination of all methods provides a conclusive picture. There is another remarkable advantage of ‘surface dust spectrometry’: Whereas remote sensing methods determine the compositional average of a certain area, a dust spectrometer is able to identify individual constituents of that area on a submicron level. Ideally, the contribution of certain minerals and compounds to a specific geological formation can be quantified. The process of creating ejecta from impacting micrometeroids is very efficient: the total mass is of the order of a few thousand times of the impactor’s mass (Koschny & Grün., 2001). The predicted density of ejecta grains in the lunar dust exosphere at an altitude of 50 km is shown in Fig. 2. In addition, during meteor showers, the ejecta population is expected to dramatically increase with a spatial distribution showing strong deviations from spherical symmetry for a duration of a few days. Fall AGU 2011 3 Z. Sternovsky P43A-1666 (Thursday) 14 LDEX + New Experiments: LDEX-2 for LADEE-2! Time-of-flight mass spectrometer. "#$%!&'$$(!$)**+!',+!-.*&/-'0!-1&)1$/21,! 34"3!!5!67!!! Fall AGU 2011 "#$%&'()*#(*&+,%"-&./0/& F. Postberg P42A-07 (Thursday) 8/&*91:9;/<.%!&'$$!$)*-%=1&*%*=! !!""#$%&! 15 &+1*""+2#&3'&4+%5#+$&*%*$)"+4#)(,#-%(+'3+%5#+",-)&+.,(%6+7%+ +:#"'$*%*#(+)-.+%&);#$%'&*#(+-##.#.+%'+.#%#&4*-#+2&'2#&%*#(+)-.+ ($ ($ ($ )$ 0$ :$ #$ 3$ #$ 0$ #$ ($ 3$ +$ *$ (& ($ Lunar Dust and Plasma Package,&./00!0123415!6785 !"#$%&'())$%*$+,$"-! !"#$%$&"'()$%*"'+",!-&-."'/0#1-2-"%'3(+/ 45'/! 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Robertson & A. Colette P41C-1634 (Thursday) Fall AGU 2011 18 Summary 1) Dust, dust charging, and dusty plasma effects are important to understand the near surface environment of the Moon and all airless objects in the solar system. 2) These issues are of interest for both basic plasma science and engineering. 3) Small-scale laboratory experiments enable the understanding of the physics, and lead to new measurement and instrument concepts. Fall AGU 2011 19