Mechanical Engineer
Outlier AI
01/2025 - Present
Increasing the real-world reasoning of generative AI models in aerospace, mechanical engineering, and space domains for the clients at Scale AI through Projects Pegasus, Starmie, and Genesis.
Engineered AI models to replicate finite element analysis performed on bearings, actuators, and transmissions with ANSYS and prepared CAD designs using SolidWorks to ensure a stress deviation of less than 2% under static and other environmental loads.
Collaborated with electronics and software engineers to test and debug spacecraft GNC module and antenna deployment mechanisms by validating mechanical interfaces and dynamic responses using MATLAB/Simulink to ensure seamless integration with control algorithms and firmware.
Authored procedure and test reports used in internal technical reviews and customer proposal packages.
Mechanical Engineer
ERETS Space
05/2024 - 12/2024
Optimized spacecraft pointing mechanisms by refining the Attitude Determination and Control System (ADCS) design, reducing mass by 6% and power consumption by 10%, enhancing efficiency for the twin CubeSat mission.
Led trade-off and cost analysis for CubeSat structural and power subsystems, identifying supplier alternatives that reduced procurement costs by 18%, cutting total system expenses by £21,000.
Reevaluated the solar array design, implementing a new deployment mechanism that reduced stowed volume by 12% while maintaining a W power budget, ensuring optimal performance in 600 km Sun-Synchronous Orbit (SSO).
Performed Monte Carlo simulations with covariance analysis and worst-case testing to ensure compliance with ECSS-E-ST-60-30C, improving pointing accuracy from 0.339° to 0.141°.
Enhanced structural reliability and thermal performance by implementing advanced finite element analysis (FEA) in Siemens NX and ANSYS, validating designs against vibration, thermal cycling, and mechanical loads.
Spacecraft Structural and Configuration Engineer
Italian Space Agency, ISAE SUPAERO, ALTEC
04/2023 - 10/2023
SEEDs (Space Exploration and Development Systems), a international collaboration between European Space Agency (ESA), Italian Space Agency (ASI), Thales Alenia Space, and ALTEC with support from Politecnico Di Torino, University of Leicester, ISAE SUPAERO .
Led the structural and configuration design of the Human Mars Lander (HML) for a four-astronaut Mars mission, collaborating with Thales Alenia Space and ALTEC, ensuring compliance with ECSS structural standards.
Optimized landing gear architecture, implementing a high-efficiency lightweight design that reduced overall mass by 3 tonnes (from 35 to 32 tonnes), improving entry, descent, and landing (EDL) safety margins.
Performed structural and risk analysis to evaluate load distribution and stress response under 6g launch loads, utilizing Siemens NX and ANSYS to ensure mission reliability and safety.
Contributed to the feasibility study of a European Commercial Space Station, executing mechanical system analysis, structural integrity evaluations, and eclipse sizing assessments, enhancing thermal load optimization strategies.
Presented key findings on spacecraft mass reduction and risk mitigation strategies at ESA and Thales Alenia Space, earning recognition for contributions toward advanced planetary lander development.
Research Assistant
Advanced Tribology Research Centre (ATRC), College of Engineering Trivandrum
08/2021 - 08/2022
Designed and developed triboelectric sensors for aerospace and renewable energy applications, optimizing mechanical configurations for enhanced energy harvesting efficiency.
Built multiphysics models of triboelectric nanogenerators using COMSOL Multiphysics, analyzing electrostatic and mechanical interactions for aerospace and renewable energy systems.
Led manufacturing, testing, and integration of triboelectric nanogenerator (TENG) devices for renewable energy harvesting, ensuring reliability and performance in extreme environments.
Engineered and fabricated a pneumatic calibration system for triboelectric material testing, enhancing precision in macroscopic parameter optimization for aerospace applications.
Conducted experimental analysis and statistical modeling on triboelectric nanogenerators, optimizing macroscopic parameters using Taguchi and ANOVA for enhanced energy harvesting efficiency.
Spacecraft Research Intern
Society for Space Education Research and Development
01/2021-03/2021
Conducted feasibility studies for propulsion and thermal control systems based on systems requirements.
Generated mission budgets and successfully developed bipropellant thrusters having sea-level exhaust velocity of 1.47m/s, achieving an overall efficiency of 93.99%.
Summarised feasibility criteria and challenges of the mission as per instructions for Critical Design Review (CDR).
Researcher (01/2024 - Present)
Chief Technology Officer (08/2021 - 08/2022)
Program Officer(10/2020 - 08/2021)
Chairperson (08/2021 - 08/2022)
Student Member (08/20219- 08/2021)
Python 3
MATLAB
Solid Works
Siemens NX
Fusion 360
CATIA V5
ANSYS
NASTRAN
ACADOS
Microsoft Office
OpenFOAM
COMSOL Multiphysics
GRAS (Geant4 Radiation Analysis for Space)
SIMULINK
CDP4 COMET
Origin 2018b
GMAT