10.1029-2018JE005826Figure211460003.pptx
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https://planetary-data-portal.org/file.xhtml?persistentId=doi:10.35003/ZUBECS/BAK5JJ
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(a) The launch position (p0), velocity (v), and angle (θ) estimation for the ejecta. The launch time (t0), landing time (tl), flight distance (tf), and landing position of the ejecta are also calculated. Note that pf defines the flight distance along the lunar surface. (b) The elliptical trajectory for each ejecta for the best fit model in this work.
提供机构：
TRR170-DB
创建时间：
2022-06-02
