M. A. Rakib, S. T. Smith, T. Tafsirojjaman | 2026 | Composite Structures
DOI 10.1016/j.compstruct.2026.120202Review state
Last reviewed
Not reviewed yet
Last approved reanalysis
No approved reanalysis yet
This paper investigates the impact performance of lunar regolith simulant-derived panels for protecting lunar structures from micrometeoroid strikes. The study evaluates Whipple shields, stuffed Whipple shields, and multi-shock shields using regolith-resin-composite (RRC) plates and regolith infill. The results provide insights into in-situ resource utilization and future experimental testing. The provided text appears to be a series of URLs related to an academic paper or document, likely from a journal or conference. The URLs point to various image and SVG files, possibly figures, diagrams, or supplementary materials. The text does not contain any meaningful content or data that can be summarized directly. It seems to be a technical artifact or a fragment of a larger document, possibly from a PDF or a web page that was not fully rendered or extracted. This paper investigates the behavior of lunar regolith simulant-derived panels under micrometeoroid impacts. The study focuses on perforation, failure mechanisms, and debris characterization. Simulant-derived panels are tested for structural integrity and damage assessment. The research contributes to the design of lunar structures
These are the records this paper contributes to the simulant, returned sample, method, and property browsers.
lunar simulant
No returned samples extracted yet.
Impact performance testing of panel systems
Mechanical testing | Lunar structure protection from micrometeoroid strikes
Impact test set-up
Mechanical | Damage assessment under micrometeoroid impacts
Damage characterisation
Mechanical | Structural integrity evaluation under impact
Compressive strength testing
mechanical testing | Construction and infrastructure
Impact testing
Mechanical testing
Shield performance analysis
Structural analysis
Material characterization
Material testing
Tensile strength testing
mechanical testing | Construction and infrastructure
Panel configuration
Preferred panel configuration
Academic Paper Identifier
S0263822326001674
Impact resistance
High
Energy dissipation
High
Material strength
High
Aerial Density
0.06-0.36 g/cm2
Material Composition
Al, RRC, BFRP, SFRP, PU foam
Impact energy
2200 J