Rocket Propulsion Engineer
Current- Led Development of Liquid Cooling System: Spearheaded a cross-functional team to design and implement a new Liquid Cooling System for the E-7 AEW&C Wedgetail, optimizing the Antenna Array. Utilized Thermal Desktop and.
- Ensured Compliance for Helium Ground Cooling on SLS EUS: Conducted in-depth heat transfer and fluid dynamics analysis, confirming adherence to helium ground chill specifications for the RL-10 engine. Successfully.
- Directed Cryogenic Valve Project: Managed the design, manufacturing, and assembly processes for a cryogenic hydrogen and helium-actuated valve, achieving complete vertical integration within an internally funded.
- Executed Testing and Qualification for KC-46A: Led FAA-required testing and qualification efforts for the KC-46A Aerial Refueler receptacle redesign. Authored the Qualified Test Report, facilitating hardware acceptance.
- Innovated Propellant Utilization Strategies: Orchestrated a high-impact Tiger Team initiative that developed innovative solutions for propellant utilization on the Exploration Upper Stage rocket, garnering recognition.
- Streamlined Interface Control Document Integration and Enhanced Propulsion CONOPs: Updated and improved the Propulsion Concept of Operations (CONOPs) for the SLS Core Stage and Exploration Upper Stage, enhancing.