At Paras Defence & Space Technologies Ltd, I led mechanical design integration for the CHIMERA 200 counter-UAV system, translating packaging, operational, and manufacturing constraints into enclosure and hardware design iterations. I developed mechanical integration concepts around computing hardware, control and HMI units, PDUs, displays, and associated electronics.
At STAR - Space Tech & Aeronautical Rocketry, I designed and developed SYLO, a static rocket-motor test platform, and produced a 17–17.9 kg physical prototype. I integrated thrust measurement, temperature and burn monitoring, weight-loss tracking, avionics access, and fire-safety provisions, supporting prototype testing and engineering documentation.
My work also includes contributing to a Triton-bound Neptune mission proposal at CONEX Research and developing sensor-integrated product and recovery prototypes. I bring experience in CAD/CAE, electronics packaging, rapid prototyping, validation, and manufacturing readiness, alongside postgraduate study in energy policy and finance.
