
NeuralinkMechanical Intern
Upcoming Internship!
Currently buildingGoblet
Mechatronics Engineering student designing and building everything cool.
I’m a Mechatronics Engineering student with over 32 months of professional engineering experience. I love designing and building hardware, electronics, and software systems, both in my free time and for work.


I’ve worked in 7 different engineering roles since 2023, from in-space propulsion to nuclear medicine to semiconductor manufacturing.
4 mo

Upcoming Internship!
4 mo

Engineered and tested in-space propulsion hardware (mostly injectors), as well as quality control processes.
4 mo

Designed, qualified, and integrated spacecraft hardware for the biggest solar sail and mirror in the world.
5 mo

Developed and deployed 5 projects, including a novel non-contact “tractor beam” for wafer handling and a performant, cost-effective, automated vacuum valve.
8 mo

Designed and manufactured components for a cyclotron-based isotope production system, conducting validation tests in-lab and building tools for streamlining production processes.
9 mo

Built a full-featured printing solution for the novel printing tech of DISC, including kinematics system, firmware, and slicer compatibility.
5 mo

Conducted high-pressure tests on hydrogen vessels and components, and developed a heating system to increase testing capabilities.
Come check out my projects!
Take the tour






Through my work and project experiences, I’ve picked up skills and expertise in multiple areas, from electronics design, to coding, to CAD modelling.
5years
4years
3years
Feel free to connect with me!
Goblet is one of the first regeneratively cooled flight engines in Canada, including both professionals and amateurs. It has to make 3.5 kN from a 3 inch chamber at an order of magnitude less mass than my previous engines, and survive multiple firings without damage.
The bulkhead is an integral part of the thrust assembly and brings both propellant feeds down from the tanks. It caps the bottom of the tanks and holds both fuel and oxidizer tubes.
Servo driven ball valves control the main oxidizer and main fuel flow, mounted directly above the engine.
A pressure tapoff through the injector means that chamber pressure can be measured directly through this pressure transducer.
A drilled-out C6 motor fires through the center of the injector to light the mixing propellant flows.
The injector was the most complex and time consuming component to design. Over 80 simulations and a year of iteration resulted in this critical-flow, like-doublet injector.
The chamber is printed in AlSi10Mg to fit a 5″ fincan. Fuel runs down the integrated inlet and back up 54 cooling channels inside the walls before reaching the injector, with a steady state of under 300C.