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A permanent, asymmetric dust cloud around the Moon - Nature

  • ️Sternovsky, Z.
  • ️Wed Jun 17 2015
  • Letter
  • Published: 17 June 2015

Nature volume 522pages 324–326 (2015)Cite this article

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Abstract

Interplanetary dust particles hit the surfaces of airless bodies in the Solar System, generating charged1 and neutral2 gas clouds, as well as secondary ejecta dust particles3. Gravitationally bound ejecta clouds that form dust exospheres were recognized by in situ dust instruments around the icy moons of Jupiter4 and Saturn5, but have hitherto not been observed near bodies with refractory regolith surfaces. High-altitude Apollo 15 and 17 observations of a ‘horizon glow’ indicated a putative population of high-density small dust particles near the lunar terminators6,7, although later orbital observations8,9 yielded upper limits on the abundance of such particles that were a factor of about 104 lower than that necessary to produce the Apollo results. Here we report observations of a permanent, asymmetric dust cloud around the Moon, caused by impacts of high-speed cometary dust particles on eccentric orbits, as opposed to particles of asteroidal origin following near-circular paths striking the Moon at lower speeds. The density of the lunar ejecta cloud increases during the annual meteor showers, especially the Geminids, because the lunar surface is exposed to the same stream of interplanetary dust particles. We expect all airless planetary objects to be immersed in similar tenuous clouds of dust.

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Acknowledgements

The LADEE/LDEX project was supported by NASA. Tests and calibrations were done at the dust accelerator facility of the University of Colorado, supported by NASA’s Solar System Exploration Research Virtual Institute (SSERVI). We are grateful for engineering and technical support from the Laboratory for Atmospheric and Space Physics (LASP), especially from M. Lankton (project manager), S. Gagnard and D. Gathright (mission operations), and D. James (calibration).

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Authors and Affiliations

  1. Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, 80303, Colorado, USA

    M. Horányi, J. R. Szalay, S. Kempf, E. Grün & Z. Sternovsky

  2. Department of Physics, University of Colorado, Boulder, 80309, Colorado, USA

    M. Horányi, J. R. Szalay & S. Kempf

  3. Institute for Modeling Plasma, Atmospheres, and Cosmic Dust (IMPACT), University of Colorado, Boulder, 80303, Colorado, USA

    M. Horányi, J. R. Szalay, S. Kempf, E. Grün & Z. Sternovsky

  4. Astronomy and Space Physics, University of Oulu, Oulu, FI-90014, Finland

    J. Schmidt

  5. Max-Planck-Institut für Kernphysik, Heidelberg, D-69117, Germany

    E. Grün

  6. Institut für Raumfahrtsysteme, Universität Stuttgart, Raumfahrtzentrum Baden Württemberg, Stuttgart, 70569, Germany

    R. Srama

  7. Aerospace Engineering Sciences, University of Colorado, Boulder, 80309, Colorado, USA

    Z. Sternovsky

Authors

  1. M. Horányi

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  2. J. R. Szalay

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  3. S. Kempf

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  4. J. Schmidt

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  5. E. Grün

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  6. R. Srama

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  7. Z. Sternovsky

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Contributions

M.H. was the instrument principal investigator, directed the data analysis, and was primarily responsible for writing this paper. J.R.S. developed the data analysis software. S.K. was responsible for the calibration of the instrument and contributed to the data analysis. J.S. led the modelling effort. E.G. and R.S. contributed to the analysis and interpretation of the data. Z.S. designed the instrument and contributed to the data analysis.

Corresponding author

Correspondence to M. Horányi.

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Extended data figures and tables

Extended Data Figure 1 Detection geometry.

A particle of velocity v is recorded by a detector of sensitive area A. The surface normal of the detector area points along the velocity vector of the spacecraft vsc. The particle enters the instrument with an angle ω measured between the instrument boresight and the relative velocity vector of the particle vscv .

Extended Data Figure 2 Systematic approximation error and its dependence on ejection parameters.

a, The calculated density for a standard set of parameters listed in Extended Data Table 1 for the model ejecta cloud12 as function of altitude (black line) normalized to the production rate N+. The density is recalculated using n = γ/(Avsc) (red line), the approach taken in this paper to infer the dust density from the measured impact rates γ, indicating an underestimate of <20% for altitudes below 100 km. b, Contour plot of the ratio of the ‘true’ model density over the recalculated density at the altitude h = 50 km, as a function of the opening cone angle of the ejecta plume ψ0 and the exponent of the power-law initial-speed distribution µ, appropriately setting the minimum speed u0, while keeping the maximum speed constant at 2vescape, maintaining a constant total kinetic energy of the ejecta particles.

Extended Data Figure 3 Comparison of observed and modelled cloud properties.

a, The dust density n(h) of the lunar ejecta cloud as function of altitude and size (colour scale). The continuous black line shows the model prediction12 using the best-fit parameters listed in Extended Data Table 1. b, The cumulative dust mass in the lunar exosphere. The continuous blue line shows the ejecta model prediction (Extended Data Table 1). c, The initial normalized vertical velocity distribution f(u) calculated from n(h) using energy conservation. The continuous line shows f(u) u−3.4 ± 0.1 matched to the data at u ≥ 400 m s−1 (altitude h ≈ 50 km). Error bars were calculated by propagating the error through the various calculations, where N is the number of detected dust impacts.

Extended Data Figure 4 Modelled flux and mass production in the lunar equatorial plane.

a, The calculated flux of interplanetary dust particles Fimp reaching the lunar equatorial region as a function of lt and t (colour coded for monthly averages). b, The mass production rate, equation (9), calculated using a model for the spatial and velocity distributions of interplanetary dust particles near the Earth16, consistent with the observed asymmetric dust cloud.

Extended Data Table 1 Parameters of the theoretical ejecta cloud model12 for the Moon

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Horányi, M., Szalay, J., Kempf, S. et al. A permanent, asymmetric dust cloud around the Moon. Nature 522, 324–326 (2015). https://doi.org/10.1038/nature14479

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  • Received: 07 October 2014

  • Accepted: 15 April 2015

  • Published: 17 June 2015

  • Issue Date: 18 June 2015

  • DOI: https://doi.org/10.1038/nature14479

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Editorial Summary

A permanent dust ring around the Moon

Before its planned demise on lunar impact in April 2014, NASA's Lunar Atmosphere and Dust Environment Explorer (LADEE) spent some seven months orbiting the Moon's equator, collecting dust particles for spectroscopic analysis. Sketches made by the Apollo 17 astronauts famously showed a lunar horizon glow, triggering suggestions that electrostatic lofting might be generating dense clouds of small dust particles high above the lunar surface. In this first report on the observations made by the Lunar Dust Experiment (LDEX) onboard LADEE, Mihaly Horànyi et al. find no evidence for such clouds. However, they have detected a permanent asymmetric dust cloud around the Moon, supplied by secondary ejecta dust particles produced by the continual surface impacts of high-speed cometary dust particles in eccentric orbits, as opposed to particles of asteroidal origin following near-circular paths and striking the Moon at lower speeds. The lunar surface is exposed to the same stream of interplanetary dust particles as the Earth, and the LDEX data show that the density of the lunar ejecta cloud increases during meteor showers such as the Geminids.