Solid
Liquid
Hybrid
01
Icarus
A modular hybrid rocket engine with swappable injector orifice, fuel grain, and nozzle, providing a controlled, repeatable testbed for studying hybrid combustion performance across varying geometries and lengths.
02
Hepheastus
A ~2 kN regeneratively cooled liquid rocket engine designed to study
high-heat-flux cooling, injector behavior, and manufacturability in
compact, reusable propulsion systems.
03
Prometheus
A regeneratively cooled aerospike rocket engine fabricated in high-temperature resin, serving as a rapid-iteration platform for thermal, structural, and geometric validation of altitude-compensating nozzles.
04
Telchines
A ~30 lbf metal AM nozzle bell engine paired with a resin-printed manifold, developed to evaluate the feasibility of partial resin construction in steady-state liquid rocket engines.
05
Jason "J-Bird"
My first major aerospace project, a Level 1 JRHPR certification rocket designed and built to demonstrate stable flight, reliable recovery, and safe high-power launch operations.
07
Zephrys
A nanocrystalline nickel–coated polymer-substrate turbopump developed to explore low-cost manufacturing pathways for high-performance pump components, with the goal of improving accessibility to liquid propulsion systems.
08
Atlas
A rigid, modular rocket engine test stand designed to restrain high thrust loads while enabling precise measurement of thrust, pressure, and thermal behavior. ATLAS serves as the foundational infrastructure for repeatable, instrumented propulsion testing across liquid, hybrid, and experimental engine systems.
09
Logos
A custom software suite that integrates propulsion design, analysis, and test data into a unified workflow, enabling constraint-driven engineering decisions from early concept through experimental validation.
