Solid, hybrid and detonation rocket propulsion models: Cantera thermochemistry, arbitrary grain burn-back, O/F control, printable nozzle CAD
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Updated
Oct 6, 2026 - Python
Solid, hybrid and detonation rocket propulsion models: Cantera thermochemistry, arbitrary grain burn-back, O/F control, printable nozzle CAD
Predicting and mitigating N2O flashing in hybrid rocket feed systems.
Valve control software for the CR25H hybrid rocket.
The board support logic for the hybrid control system mission control box running on NuttX.
Hybrid pad control center board support for NuttX.
Steady-state analytical model of polymer surface regression by depolymerization into vapor-phase monomer
Regression rate of a solid polymer fuel in a counterflow diffusion flame, computed with Cantera
Transient multiphysics model of solid polymer fuel regression: conduction, melting, depolymerization, evaporation, and a moving surface (finite differences + RK4)
A modular aerospace engineering platform for hybrid rocket conceptual design, simulation, analysis, documentation, manufacturing preparation, validation, and AI-assisted engineering workflows.
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