SearcharxivSearch

arXiv subjects

Mavia Anjum

Publications and source records attributed to Mavia Anjum.

2 recordsLinked to original sources

Geochemical Hazard Assessment of Martian Regolith for Future Human Exploration

As human missions to Mars move from concept to planning to reality, a systematic quantitative health risk assessment of martian regolith exposure has become critically important. This study presents a comprehensive multi-element, multi-pathway health hazard analysis of martian regolith for a 70 kg adult astronaut on an 18-month surface mission, using bulk silicate Mars geochemical data and Earth Upper Continental Crust reference values as baseline comparators. We computed Average Daily Dose, Hazard Quotient, Hazard Index, Enrichment Factor, Ecological Risk Factor, and Incremental Lifetime Cancer Risk across all three exposure pathways (oral ingestion, inhalation, and dermal contact) for toxic and heavy metals, under four filtration scenarios (0%, 25%, 50%, 95%). Results demonstrate that Cr and Co represent the most critical non-carcinogenic hazards, exceeding the regulatory threshold (HI > 1) even at 50% filtration, while Cr also poses the most significant carcinogenic risk, near the $10^{-4}$ regulatory threshold level. At least 92% regolith filtration efficiency is required to reduce Cr to acceptable non-cancer hazard levels. Nickel exceeds the acceptable cancer risk threshold of $10^{-6}$ at all filtration levels below 95%. No element other than Cr and Co exceeds HI = 1 in the unfiltered scenario, although Fe, Ni and Mn approach concerning levels. These results establish that a minimum 95% High-Efficiency Particulate Air (HEPA)-grade filtration efficiency combined with active chemical sorption is required for acceptable Cr and Co short term exposure and Cr, Ni long term exposure management. This study provides a pathway-specific quantitative risk framework applicable to habitat air quality standards and EVA suit specifications for Mars surface operations

q-bio.OT

Assessment of the 5 August 2026 Falcon 9 Upper-Stage Lunar Impact: Energetics, Crater Scaling, and Comparison with LRO Observations

The objective of this study was to characterize the human-made object that impacted the Moon on 5 August 2026, to estimate the dimensions of the crater it produced, and to compare the estimates with the crater subsequently measured by the Lunar Reconnaissance Orbiter (LRO). The impactor was the discarded upper stage of a SpaceX Falcon 9 rocket, which struck the surface near Einstein crater at a velocity of 2.43 km/s. The kinetic energy and linear momentum of the impactor were calculated, and the crater diameter was estimated using pi-group scaling relationships and measured rocket-body impacts as empirical analogs. The kinetic energy of the impactor was found to be 1.18 x 10^10 J, equivalent to approximately 2.8 tonnes of TNT. Compact-body pi-group scaling yielded a final rim-to-rim diameter of 46-57 m, and the empirical analogs yielded 26-27 m, leading to a pre-observation preferred estimate of 25 m within a range of 20-30 m. Between 11 and 12 August 2026, LRO imaged a crater approximately 18 m in diameter and less than 3 m deep. The results revealed that the compact-body scaling overpredicted the observed diameter by a factor of 2.6-3.2, whereas the empirical-analog method overpredicted it by 39-50%. When the nearest-mass analog was applied as a single crater rather than as a double crater, the estimated diameter was approximately 18 m, in close agreement with the observation. It was found that the hollow and elongated geometry of the stage, rather than a single equivalent bulk density, is the principal factor governing the crater size. This study provides a direct comparison of impact-scaling methods against a measured artificial lunar crater.

astro-ph.EP