Variable engine gaseous test stand

VEGAS

Boston University Rocket Propulsion Group

    • Design modular frame: Create a versatile frame that allows easy interchangeability of components for different engine types.

    • Modular mounts: Design adjustable engine, fuel tank, and propulsion mounts for quick engine swaps and adaptability.

    • Load cell integration: Incorporate high-precision load cells for accurate thrust measurement, with multi-axis support for vertical and horizontal force.

  • Structures Engineer

    • Onboarding – Hybrid Rocket Engine Development (Sep 2024 – Dec 2024)

    • Structures Engineer – VEGAS (Feb 2024 – Present)

    • Solidworks

    • Structural Finite Element Analysis (FEA)

    • Milling

    • Mechanical Design & Analysis

    • Machine Design

    • Designed and built a modular nozzle fixture integrating with existing fluid and fire-extinguishing systems.

    • Eliminated torque on the thrust-measuring load cell, ensuring accurate force readings and analysis for new engine systems.

    • Contributed to next-generation liquid propulsion development, supporting RPG’s efforts to become the first university team to launch a liquid-fuel rocket into space.

Horizontal Test Stand (HTS) - Predecesseor of VEGAS. I am currently designing avionics structures for its continued use.