Nozzle Generation
Define and generate nozzle geometries for liquid propulsion systems with practical design inputs.
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Chimp Propulsion Analysis (CPA)
CPA is a comprehensive tool for liquid rocket nozzle generation and regenerative cooling heat transfer analysis, with clear plotting and preview workflows to support faster engineering decisions.
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Regenerative Cooling Analysis
Run thermal analysis for chamber/nozzle cooling channels and inspect thermal headroom quickly.
Engineering Visualization
Use plotting outputs and previews to interpret solver behavior and communicate design status.
Who Uses CPA
Propulsion engineers, student launch teams, and R&D groups building liquid-fueled engines that need fast sizing and thermal analysis feedback loops.
Join the Waitlist
CPA checkout is being finalized. Join the waitlist for launch access and release updates.
Toss Payments integration is prepared in the codebase and will be enabled once commercial details are ready.