▪ Analyzed, troubleshooted, and repaired software anomalies identified by NASA flight engineers to simulate all aspects of day-to-day operations from predictive ephemeris generation to backup orbit determination using various TDM files▪ Performed end-to-end Systems Development Life Cycle process from requirements creation to software delivery, implementation and maintenance▪ Developed, maintained, and updated Oracle SQL Database to have a 100% operational up-time for testing▪ Contributed to the advancement of multiple system platforms to minimize the processing time by over 50% to maximize the operations capabilities for real-time applications ▪ Identified, analyzed, and resolved system design weaknesses in critical satellite flight dynamics software to analyze flight products and ephemeris data ▪ Utilized Jenkins Shell Script to develop an automated test machine to analyze over 75% of existing software processes ▪ Designed complex test procedures to verify 100% of the software requirements for performance analysis and systems verification during factory acceptance testing

* Utilized SolidWorks FEA simulations on the rocket test stand to run a nonlinear dynamic simulation under 1500lbs of thrust for a burn time of 10 seconds to analyze the stress distribution and potential material failure * Organized weekly status reports for the team, and presented the weekly progress to the project manager.* Collaborated with team members in order to efficiently design the nozzle and combustion chamber that will fit with the team's cooling mechanism* Analyze the effects of regenerative cooling for the combustion temperature in the post combustion chamber and the nozzle using Paraffin fuel and Nitrous Oxide as the coolant* Ran Solidworks simulations to test for material failure on the rocket test stand under different conditions* Program Load Cells to operate with Arduino software* Performed detailed thermal calculations with the help of NASA’s CEA program to determine the hottest temperature on the rocket

* Fabricated a hot-wire anemometer using platinum Wollaston wires to analyze the effects of boundary layer separation on an airfoil under various flight conditions* Performed wind tunnel calibration tests by increasing the wind velocity at a controlled rate of 2 - 5 m/s to ensure accurate data collection under test conditions

* Hands on experience with design, build and test* Designed with materials such as Carbon Fiber, Peel Ply, Balsa Wood, Breather cloth, Epoxy, Polystyrene Foam and more* Fabricated propellers using bidirectional and unidirectional carbon fiber, balsa wood and epoxy to hold them together on top of a fiberglass mold and then implementing a vacuum bagging method in order to harden the epoxy* Assembled an H-Tail and tested the movement of the tail under flight conditions using wires in order to calculated the angle of deflection* Assisted in the development of the wing ranging from Mylar testing to attaching the leading and trailing edges