

February 2026 monthly summary for PURPL-Purdue/Turbopump focusing on feature delivery and analytics enhancements. Two primary features delivered; 1) naming and unit consistency improvements for impingement distance, and 2) a new turbopump analysis script for pressure drops and injection angles. No major bugs fixed this month. Overall impact: clarified naming, standardized units, and expanded modeling/analysis capabilities that support more accurate simulations and informed design decisions. Demonstrated skills in Python scripting, YAML/config refactoring, unit handling, and version-control traceability.
February 2026 monthly summary for PURPL-Purdue/Turbopump focusing on feature delivery and analytics enhancements. Two primary features delivered; 1) naming and unit consistency improvements for impingement distance, and 2) a new turbopump analysis script for pressure drops and injection angles. No major bugs fixed this month. Overall impact: clarified naming, standardized units, and expanded modeling/analysis capabilities that support more accurate simulations and informed design decisions. Demonstrated skills in Python scripting, YAML/config refactoring, unit handling, and version-control traceability.
January 2026 monthly summary for PURPL-Purdue/Turbopump. Delivered two injector design parameter calculators to accelerate injector optimization and parameterization for RP1/LOX. Implemented: (1) a quadlet manifold parameter calculator focusing on propellant mass flow distribution and injector design optimization, and (2) a triplet injector calculator providing detailed injector parameters (orifice diameter, exit velocity, and pressure drops) for RP1 and LOX. Implemented changes are tracked in two commits: cee5eb88d7358971bab4ad205c97b0d3e60a6354 and ecfba40e90917697541479de237c83f19e5185df (Add files via upload). This work establishes a reusable design automation foundation, enabling faster, data-driven injector studies and design iterations. No major bugs reported; repository state remains stable.
January 2026 monthly summary for PURPL-Purdue/Turbopump. Delivered two injector design parameter calculators to accelerate injector optimization and parameterization for RP1/LOX. Implemented: (1) a quadlet manifold parameter calculator focusing on propellant mass flow distribution and injector design optimization, and (2) a triplet injector calculator providing detailed injector parameters (orifice diameter, exit velocity, and pressure drops) for RP1 and LOX. Implemented changes are tracked in two commits: cee5eb88d7358971bab4ad205c97b0d3e60a6354 and ecfba40e90917697541479de237c83f19e5185df (Add files via upload). This work establishes a reusable design automation foundation, enabling faster, data-driven injector studies and design iterations. No major bugs reported; repository state remains stable.
December 2025 monthly summary for PURPL-Purdue/Turbopump focused on delivering advanced injector design tooling, expanding data management capabilities, and laying groundwork for scalable design iterations. The month emphasized business value through improved accuracy, faster iteration, and better data portability for injector design runs.
December 2025 monthly summary for PURPL-Purdue/Turbopump focused on delivering advanced injector design tooling, expanding data management capabilities, and laying groundwork for scalable design iterations. The month emphasized business value through improved accuracy, faster iteration, and better data portability for injector design runs.
November 2025 monthly summary for PURPL-Purdue/Turbopump. Delivered the Injector Parameter Calculator enabling automated calculation of design parameters for liquid rocket injector design, including mass flow rates, velocities, and injector geometry; extended calculations to cover angles and refined pressure (y-component) calculations; improved output formatting and added documentation/metadata for usage and maintenance. Performed code refactors for clarity and modularity to support future enhancements. Delivered six commits across iterations to improve functionality and maintainability.
November 2025 monthly summary for PURPL-Purdue/Turbopump. Delivered the Injector Parameter Calculator enabling automated calculation of design parameters for liquid rocket injector design, including mass flow rates, velocities, and injector geometry; extended calculations to cover angles and refined pressure (y-component) calculations; improved output formatting and added documentation/metadata for usage and maintenance. Performed code refactors for clarity and modularity to support future enhancements. Delivered six commits across iterations to improve functionality and maintainability.
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