Sara Schmidheiser
Lead R&D Engineer @ Helion
About
I am a systems-focused engineer with a proven track record of rapidly learning complex technologies and applying that knowledge to drive progress and problem-solving in high-stakes environments. Over the course of my career, I have built a strong foundation in understanding, operating, and troubleshooting intricate systems, which has allowed me to thrive in both aerospace and energy sectors. For over 3 years, I contributed to the success of SpaceX's Raptor engine during a critical phase of its development. As an integral member of the propulsion development team, I was able to dive deep into the details of engine operation and help push the boundaries of space exploration technology. Currently, I am part of the test operations team at Helion Energy, where I’m focused on mastering the operation of plasma Field Reversed Configuration (FRC) machines. My goal is to contribute to the success of Polaris and help usher in the future of energy by generating power from nuclear fusion. With my adaptability, technical expertise, and commitment to continuous learning, I am driven by the opportunity to work on groundbreaking technologies that shape the future of both space and energy.
United States
Greater Seattle Area
Aviation & Aerospace
Microsoft Word, Microsoft Office, Microsoft Excel, Autodesk Inventor, SolidWorks, Matlab, PowerPoint, Leadership
Experience

Graduate Student Researcher
Atlanta, GA
• Operated an RQL-type combustor, with typical conditions up to 800 kPa and 2000K, to determine the mechanism of combustion instability and acoustic tone generation in currently operating engines. • Used MATLAB to develop processing algorithms to relate pressure data and flame dynamic modes by accomplishing an extensive image decomposition analysis. • Designed, set up, and executed a unique testing campaign to further identify the interaction between a swirl-stabilized liquid fuel injector and acoustic instability. • Optimized and tested a gaseous fuel, reacting jet-in-crossflow, combustor at 20 g/s and 1500K, designed to simulate a staged combustor. • Designed and manufactured a bluff-body fuel injector to study the interaction of multiple jets in a crossflow, modeling fuel injection systems in an afterburner. • Used CHEMKIN and chemical equilibrium programs to calculate parameters including flame temperature and ignition delay. • Directed and supported undergraduate students who contributed to experimental work and technical analysis.

Combustion Diagnostics Intern
Dayton, Ohio Area
• Studied a bluff body, afterburner combustor operating at 2000K and 250 g/s using flame imagery and pressure data to determine the effect of fuel characteristics like cetane number on the amplification of combustion instability. Results used to inform aircraft operating windows. • Developed flame tracing algorithm to track the progress of instability onset as a function of equivalence ratio. • Responsible for setup, calibration, and operation of laser-based diagnostics equipment, and installation of pressure transducers. • Designed hardware and software for a novel hyperspectral IR surface temperature probe designed to function in sooty combustion environments in which other measurement techniques are unreliable.

Undergraduate Research Assistant
Atlanta, Georgia, United States
• Single-handedly performed data reduction on experimental test campaign results including flowfield velocity and flame imagery. • Responsible for daily calibration of 6-camera setup and alignment of a 3-laser optical system, as well as flow seeding hardware as an integral team member in a first-of-its-kind data collection campaign. • Aided in setup modifications like flow metering through use of critical orifice sizing, fuel substitutions, and repair of optical panels. • Improved data analysis tools by debugging Labview VI and developing comparative data processing tool in MATLAB.

Propulsion Engineering Co-op
Atlanta
• Worked alongside full-time engineers to continuously improve the reliability of Delta’s jet engines fleet for four semesters. • During final work term, acted as the sole workscope engineer for the JT8D-219 engine by authoring repair and investigative instructions for the engine shop, working closely with engine mechanics. • Conducted investigation on the shop floor to identify the cause of damage to engine onboard computer and implemented preventative actions, resulting in a projected savings of $320,000/year. • Developed fleet-wide project to identify and prevent the cause of in-flight engine shutdown event, which is currently being implemented, resulting in improved reliability ratings.

Lab Assistant
Aerospace Systems Design Lab at Georgia Tech

Student Assistant
Greater Atlanta Area
Ensure groups renting event space have all contracted amenities and support services. As a student assistant I open and close the building, setup and take down event equipment including audio/visual equipment, greet and assist event attendees, and address all concerns or questions during events ranging from information sessions to weddings.
Sara Schmidheiser's Contact Information
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