The LCROSS Cratering Experiment

Details The LCROSS Cratering Experiment The LCROSS Cratering Experiment

Oct 2010

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2010sci...330..468s&link_type=abstract

Science, Volume 330, Issue 6003, pp. 468- (2010).

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Scientific paper

As its detached upper-stage launch vehicle collided with the surface, instruments on the trailing Lunar Crater Observation and Sensing Satellite (LCROSS) Shepherding Spacecraft monitored the impact and ejecta. The faint impact flash in visible wavelengths and thermal signature imaged in the mid-infrared together indicate a low-density surface layer. The evolving spectra reveal not only OH within sunlit ejecta but also other volatile species. As the Shepherding Spacecraft approached the surface, it imaged a 25- to-30-meter-diameter crater and evidence of a high-angle ballistic ejecta plume still in the process of returning to the surface—an evolution attributed to the nature of the impactor.

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