Space Colonization and Habitation, Sintering, Mechanical and Materials Characterization, Extra-terrestrial in-situ resource utilization, Fracture Mechanics, Mechanical Behavior of Materials, and Composite Materials.
Mechanical testing - Universal Testing Machine (Compression, tensile, flexural), Impact testing, SHPB, etc
Materials Testing - Scanning Electron Microscopy, X-ray diffraction, Micro-CT, FTIR, TGA, etc
Software's - MATLAB, PYTHON, ANSYS, CATIA, AutoCAD, Blender, Origin, ImageJ, LATEX
As part of the ANR HotTips project, I will be working on the following:
Implementing a new experimental technique to measure local crack tip temperatures;
Conducting fracture experiments on polymeric glasses, artificial rocks, and silicate glasses, from low-speed to high-speed fracture regimes.
Human curiosity for the profound secrets of space may lead to the establishment of extraterrestrial communities. Mars and the moon, due to their proximity to Earth, have been recognized as unprecedented supplies of processable materials, making them the favored alternatives for space organizations throughout the world to build temporary buildings and observatories. These dwellings must be developed on the moon/Mars using in situ resources in order for space exploration to be practical and sustained. The fundamental challenge in this attempt is the consolidation of unbonded fine regolith particles into a structure with significant mechanical integrity. My research investigates various consolidation methods for manufacturing of construction materials and joining them to form structures in an extraterrestrial environment, providing insights for constructing robust and sustainable construction processes.
The first consolidation method investigated is muffle furnace-based sintering, which mimics firing processes for producing commercial clay-based bricks. A protocol for both green and brown part (bricks) production is first established, followed by evaluation of compressive (unconfined) strengths of the produced bricks. The micromechanics of particle coalescence in solid state sintering of lunar regolith is evaluated using techniques derived from classical ceramic sintering. Additionally, consolidation of regolith simulants rich in glassy basalt is studied using both solid state and liquid state sintering. Final failure modes via multiple crack nucleation and growth are also investigated. Production of bricks with compressive strengths of upto 55 MPa is demonstrated via the sintering process.
The second method involves the use of biopolymer binders to consolidate lunar and Martian regolith simulants, termed biopolymer regolith composite (BRC). The use of guar and xantham gum is investigated, resulting in consolidated bricks with compressive strengths up to 15 MPa. Additionally, the consolidates are demonstrated to be resilient to large environmental changes, including thermal fluctuations and ultra-high vacuum. While the final consolidated brick strengths are lesser than that with sintering, the process is easily scalable and is significantly less energy intensive.
The third method involves the use of microbial-induced calcite Precipitation (MICP) for creating consolidates, termed space bricks, using lunar and Martian regolith simulants. Incorporating Sporosarcina pasteurii bacteria, a ureolytic pathway is initiated. Adding guar gum and NiCl2 significantly enhances compressive strength, making the bricks comparable to commercially used mud bricks. Including glass fiber, while slightly reducing strength, enables machinability for precise shaping without specialized molds. This approach, validated through detailed microscopy and analytical techniques, presents a promising avenue for robust extra-terrestrial structures, aligning with in situ resource utilization principles.
Finally, the use of BRC as a lower strength cementing material for joining sintered bricks in the form of a wall is studied. Failure mechanisms at the wall level, including crack paths and potential Cook-Gordon type strengthening are investigated under quasi static tension/ compression tests as well as high-velocity projectile impact.
Aircraft wings, essential for flight, are complex structures made of spars, ribs, and skin. In this project, a wing was modeled in CATIA V5 and analyzed for stress and strain using ANSYS Workbench. Various composite laminates with different fiber orientations were tested, with orientations selected via MATLAB analysis. CFRP laminates were manufactured and subjected to mechanical tests, including tensile, compressive, flexural, and impact strength assessments. Results showed that mixed laminates offered up to 23% better tensile strength and 26% higher flexural strength compared to pure laminates, while symmetric laminates excelled in compression strength by up to 40% over asymmetric types.