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Quadrotor UAV propulsion system analysis using AIML - T/W ratio, power consumption, battery sizing and payload optimisation. Arduino Uno gesture-to-flight-command pipeline with obstacle avoidance. Python + Embedded C.
Conceptual design and analysis of a liquid-propellant rocket engine for orbital launch vehicles. Presents key specs (chamber pressure, nozzle expansion, thrust-to-weight), propellant/material selection (LOX/RP-1 & LOX/LH₂), cycle considerations, and computational workflows for engine sizing, sweeps and trade-off studies.