TY - JOUR
T1 - Lunar impact ejecta flux on the Earth
AU - Castro-Cisneros, Jose Daniel
AU - Malhotra, Renu
AU - Rosengren, Aaron J.
N1 - Publisher Copyright:
© 2025 Elsevier Inc.
PY - 2025/9/15
Y1 - 2025/9/15
N2 - The transfer of material between planetary bodies due to impact events is important for understanding planetary evolution, meteoroid impact fluxes, the formation of near-Earth objects (NEOs), and even the provenance of volatile and organic materials at Earth. This study investigates the dynamics and fate of lunar ejecta reaching Earth. We employ the high-accuracy IAS15 integrator within the REBOUND package to track for 100,000 years the trajectories of 6,000 test particles launched from various lunar latitudes and longitudes. Our model incorporates a realistic velocity distribution for ejecta fragments (tens of meters in size), derived from large lunar cratering events. Our results show that 22.6% of lunar ejecta collide with Earth, following a power-law C(t)∝t0.315, with half of the impacts occurring within ∼10,000 years. We also confirm that impact events on the Moon's trailing hemisphere serve as a dominant source of Earth-bound ejecta, consistent with previous studies. Additionally, a small fraction of ejecta remains transiently in near-Earth space, providing evidence that lunar ejecta may contribute to the NEO population. This aligns with recent discoveries of Earth co-orbitals such as Kamoóalewa (469219, 2016 HO3) and 2024 PT5, both exhibiting spectral properties consistent with lunar material. These findings enhance our understanding of the lunar ejecta flux to Earth, providing insights into the spatial and temporal patterns of this flux and its broader influence on the near-Earth environment.
AB - The transfer of material between planetary bodies due to impact events is important for understanding planetary evolution, meteoroid impact fluxes, the formation of near-Earth objects (NEOs), and even the provenance of volatile and organic materials at Earth. This study investigates the dynamics and fate of lunar ejecta reaching Earth. We employ the high-accuracy IAS15 integrator within the REBOUND package to track for 100,000 years the trajectories of 6,000 test particles launched from various lunar latitudes and longitudes. Our model incorporates a realistic velocity distribution for ejecta fragments (tens of meters in size), derived from large lunar cratering events. Our results show that 22.6% of lunar ejecta collide with Earth, following a power-law C(t)∝t0.315, with half of the impacts occurring within ∼10,000 years. We also confirm that impact events on the Moon's trailing hemisphere serve as a dominant source of Earth-bound ejecta, consistent with previous studies. Additionally, a small fraction of ejecta remains transiently in near-Earth space, providing evidence that lunar ejecta may contribute to the NEO population. This aligns with recent discoveries of Earth co-orbitals such as Kamoóalewa (469219, 2016 HO3) and 2024 PT5, both exhibiting spectral properties consistent with lunar material. These findings enhance our understanding of the lunar ejecta flux to Earth, providing insights into the spatial and temporal patterns of this flux and its broader influence on the near-Earth environment.
KW - Asteroids
KW - Dynamics
KW - Moon
KW - Near-earth asteroids
UR - https://www.scopus.com/pages/publications/105003927840
UR - https://www.scopus.com/pages/publications/105003927840#tab=citedBy
U2 - 10.1016/j.icarus.2025.116606
DO - 10.1016/j.icarus.2025.116606
M3 - Article
AN - SCOPUS:105003927840
SN - 0019-1035
VL - 438
JO - Icarus
JF - Icarus
M1 - 116606
ER -