• Lead technical expansion of company customer base by 100% through leading the investigation of different Mission Extension Pod (MEP) variants• Improved program efficiency and organized technical details through MS Project, task management boards, scope prioritization, and cost account management• Demonstrated peer-to-peer leadership and delegation to enable increased workload• Determined MEP variant technical feasibilities by working with multiple subsystem subject matter experts• Personally recognized by Senior Management for a successful deliverable and noted obvious efforts put into deliverables

• Developed multiple multi-million dollar proposals with customer by evaluating requirements, statement of work, and basis of estimates• Optimized flow of proposal process by developing visual representation of the entire bid & proposal effort

• Spearheaded state machine diagrams for multiple subsystems to establish a program wide understanding of subsystem states and modes• Lead the development of MEP States and Modes in multiple formats to provide a comprehensive viewpoint of subsystem states throughout the mission lifecycle• Collaborated on creating mission operations documents for multiple subsystems

• Lead technical expansion of company customer base by 100% through leading the investigation of different Mission Extension Pod (MEP) variants• Improved program efficiency and organized technical details through MS Project, task management boards, scope prioritization, and cost account management• Demonstrated peer-to-peer leadership and delegation to enable increased workload• Determined MEP variant technical feasibilities by working with multiple subsystem subject matter experts• Personally recognized by Senior Management for a successful deliverable and noted obvious efforts put into deliverables

• Coordinated and developed a complex cross-IPT key capability sequence from scratch, featured at three separate presentations with high customer visibility• Conducted architecture modelling and trade study discussions and efforts for a payload enhancement from both Ground and Space perspectives• Pioneered a DoDAF 1.5 metamodel to accelerate overall understanding of modelling architecture and efficiencies• Led multiple tiger team working groups with up to 15 different engineers of various levels to develop capability sequences and create a collaborative knowledge repository with traceability

● Released a comprehensive initial coordinate systems for the Next Gen Polar program● Created multiple traceability, comments, and tasks matrix documents for ease of access while working and for future references after passing it off

● Led and managed a team of multi-disciplinary fields to architect all major subsystems of a lunar rover from scratch● Developed system requirements, architecture, and risk analysis to improve the organization of subsystem workflow● Significantly improved and increased the accuracy of a rapid complexity-based cost index assessment analysis derived from NASA Jet Propulsion Laboratory● Developed a 42-page lunar rover concept proposal to NASA’s RASC-AL Evaluation Committee

Physically modified steel tower units, guy-wire, and solar panel assemblies for ease of integration in AntarcticaCreated CAD and ICDs for high voltage mass spectrometer housingDeveloped systems-level process flow charts and identified system drivers for electrostatic radiation shielding

● Established new schedule flow-charts to help keep members diligent and on-track ● Improved work-time utilization by optimizing online workspace and documentation● Initiated and lead specialist teams to resolve critical issues and resolved action items within 6 weeks● Cut meeting times by 50% while maintaining discussion of critical items

• Sole mechanical team member; created a TRL-6 balloon launch design to accommodate an experimental battery for near-space testing conditions• Designed in Creo and performed transient thermal analysis in Solidworks with accurate simulations• Created a program in Matlab that characterized internal payload atmospheric conditions• Developed new process for polystyrene integration• Successfully launched and recovered balloon experiment

• Used Patran and Nastran to perform Static, Modal, Modal Frequency, and Modal Transient Response analysis to determine mirror deformation under inertial loading and microthruster noise.• Used SigFit to decompose mirror deformation into Zernike coefficients to determine Line-of-Sight and Wavefront Error• Improved primary mirror support system to allow structure to satisfy launch load requirements• Explored alternative designs to satisfy different launch vehicles

• Managed entire CubeSat for integration with other system components, functionality of mechanisms, CTE and tolerance interfaces, and other various system level tasks,• Used SolidWorks to optimize a 3U CubeSat, with appropriate mounts, holes, and PCB boards; collaborated with all other subsystems to decide optimal spacing and integration

Helped on the assembly, integration, testing, and some design for the Remote Sensing Mast and Chassis Bracket Analysis for the Mars 2020 project.