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Explore lunar exposure dynamics to Earth's plasmasheet, analyze past observations, and discuss implications for lunar exploration and mission planning. Investigate dust transport, surface charging risks, and propose future steps for improved modeling and data collection.
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The exposure of the Moon to the Earth’s plasmasheet Mike Hapgood STFC Rutherford Appleton Laboratory (M.Hapgood@rl.ac.uk)
Plasmasheet CONTEXT • Moon crosses magnetotail around Full Moon • ~4 to 5 days per month • Xgse ~ - 60 Re • Sometimes encounters dense hot plasma of the plasmasheet • Lunar surface can gather charge in these conditions • E.g. observed by Lunar Prospector Summary of 50 keV electrons seen by Cluster
When is Moon in plasmasheet? • Zmoon ~ Zsheet • Zsheet set by dipole tilt • annual ± 4 Re, + in northern summer • also smaller diurnal motion • also variation with Ygse • Zmoon set by inclination of Moon’s “orbit” • annual motion ± 5.5 Re • phase varies with precession of Moon’s orbit (18.6 year cycle) June Neutral sheet Ecliptic plane AN DN Moon’s orbit inclined by 5 Nodes precess 360 in 18.6 years
Detailed calculation • Apply to period 1960-2030, with 1h resolution • 70 year run to cover several precession cycles • Include mix of past and future dates • Take plasmasheet as | Zmoon - Zsheet| ≤ 2 Re • Moon position • Inertial position (RA, Dec, R) from IDL Astronomy Library at NASA Goddard • Convert to GSE using local transformation library • Plasmasheet location • Use Tsyganenko 1998 neutral sheet model (to X=-100 Re) • Assume Vsw=400 km s-1, θSW=0, By =0 (limited real data – subject for future work)
Exposure per monthraw monthly25-month meanhalf-yearly envelopes
Model overview • Marked variation in lunar exposure over 18 year precession cycle • Driven by phase difference between Z variation of plasmasheet and of full Moon • In-phase near cycle maximum • Best match slightly off maximum (ΔZmoon > ΔZsheet) • Antiphase at cycle minimum • Peaks around 1976/1980, 1995/1999, 2013/2017 • Are past peaks supported by observations?
What do observations report? • No long-term observations • But spot observations are suggestive • Lunar Prospector (1998-9) observed upward e- beans indicative of surface charging to several kV associated with PS and SEP (Halekas et al, GRL, 2005 & 2007) • Lunar exosphere (Na) observed during 5 eclipses in 1993-2000, exosphere strongly enhanced in cases close to PS crossings (Wilson et al, GRL, 2006) • What about Apollo? • Missions all on dusk flank (First Quarter moon phase) • Little or no overlap with plasmasheet
Why does this matter? • Dust transport • dust is major environmental issue for lunar exploration • levitated dust observed by Apollo & precursors (e.g. images, visual reports, surface dust experiments) • electrodynamics is key to dust transport • Charging of equipment on surface • Similar to spacecraft charging • Risk of discharge on landing • Potential drop over Debye length above surface? • Similar risk exists for aircraft in Earth’s atmosphere?
Next steps • Explore impact of By on plasmasheet model • Focus on periods with good IMF data • Improve time resolution of model • Work in progress • Look for other data sources: • Anything from Apollo surface measurements? • Geotail and Wind lunar passes • SMART-1, Chandryaan, Lunar Reconnaissance Orbiter • Highlights need for better plasmasheet models • Need to model Z variation • Old models from ISEE give X & Y, Cluster gives Z
Conclusions • Dynamical properties of Moon’s orbit imply 18-year cycle in lunar charging • Related to cycle of eclipse occurrence • Should consider in long-term mission planning • Experience at minimum (e.g. now) is not a guide to conditions at maximum • Needs further work • Explore role of By in model • Search for additional observational data • New measurements to monitor e- flux and charging (but can this be done on a penetrator?) MoonLite concept