A tool for preliminary design and regenerative cooling modelling of liquid propellant rocket engines
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Updated
Oct 25, 2024 - MATLAB
A tool for preliminary design and regenerative cooling modelling of liquid propellant rocket engines
Open Computational Architecture for Aerospace Hardware
Frame-locked 34-second sectional anatomy of a methalox full-flow staged combustion engine. Raptor-inspired conceptual model with no invented pressures, speeds, or angles.
34-second frame-locked schematic of Full-Flow Rocket Engine. Explanatory only, not a certified reference.
Parametric luquid engine design tool , requirements become inputs and then they become constraints. They get sized and the output is a 3D-printable engine
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