Engineering Engineer

ANTHONY S. MISHEK

*** ****** ** **, *********** MN 55413 651-***-**** *******@*****.***

Objective: Highly motivated, decisive and result-oriented individual with a passion for space exploration seeking a position as an Engineer inside a company dedicated to pushing the boundaries of space flight.

EDUCATION

University of Minnesota-Twin Cities, Twin Cities, MN, United States

BS in Aerospace Engineering and Mechanics (GPA: 3.0) May 2015

CORE COMPETENCIES

●In-depth knowledge of the applications of physics and mathematics in designing aero/mechanical structures.

●Comprehensive knowledge of the theories, practices, and techniques of engineering.

●Strong data analysis skills.

●Strong analytical and troubleshooting skills.

●Outstanding communication skills blended with strong technical presentation.

SOFTWARE SKILLS

●Matlab/Simulink: Completed full Matlab Simulation course in undergraduate. Used Matlab extensively throughout my undergraduate to analyze and model data collected from wind tunnel tests, to develop a stability augmentation system (SAS) for a model airplane, create orbital simulations, and in many other projects and assignments.

●C/C++: Completed C/C++ software engineering course during undergraduate studies.

●SolidWorks/CAD: Completed SolidWorks Essentials training course provided by Alignex.

●Microsoft Office Suite (Word, Excel, PowerPoint, Office).

WORK HISTORY

SRS Aviation, Prior Lake, MN, United States

Aerospace Engineer, September 2015- Present

●Engineering duties: Reverse engineering and creating CAD models and detailed drawings of aircraft flight control components using SolidWorks, and preparing technical documents for FAA Parts Manufacturer Approval (PMA) and Supplemental Type Certificate (STC) submissions for certification of new parts. Ensure SRS parts, drawings, manufacturing processes, and technical documents comply with current FAA regulations, and perform FEA analysis on critical (i.e. life-limited) components that SRS Aviation has made major modifications to. Leader of multiple PMA projects (2-3 person team), which involves creating project certification plans, assigning tasks, and being a primary contact to answer questions and provide progress reports with FAA engineers and any DERs (Designated Engineering Representatives) involved in the projects.

●Quality Control duties: Inspect and ensure fabricated parts comply with ISO 9001, AS9100 (for military contracts), and internal quality standards for product development and manufacturing. Methods used for quality assurance include inspecting dimensional tolerances of manufactured parts to ensure parts conform with SRS drawings, Rockwell hardness and conductivity testing to ensure parts were heat treated correctly, and reviewing all manufacturing work travelers to ensure all other steps in manufacturing processes were completed correctly.

ADDITIONAL EXPERIENCE/PROJECTS

Senior Design Project sponsored by Orbital ATK.

●Project goal was to design a self-contained soft recovery system for air dropped munitions testing for ATK.

●Set requirements and objectives with ATK.

●Developed Gantt chart to organize tasks and deadlines.

●Conducted at preliminary design review (PDR), comprehensive design review, and a build readiness review.

●Developed testing matrix with complete test plans, test descriptions, and test reports to conduct tests for project components.

●Simulated flight path of munition using Matlab.

●Conducted failure mode and effects (FMEA) analysis.

●Completed a technical write up reviewing the entire project.

●Orbital ATK plans to implement our design into future testing Hatchet munition.

Liquid Fuel Rocket Engine Campus Club

●Campus club devoted to designing and building a liquid propellant (GOX/Kerosene) rocket engine.

●Rocket engine was designed to have 100N of thrust and a burn time of 30 seconds.

●I was a member of the propulsion sub-team, which involved using thrust equations to determine combustion chamber pressure, exit nozzle area, pressure, and temperature required for our desired thrust. Also calculated fuel line pressures to determine what material/size can withstand the pressures, and the fuel/oxidizer mixture ratio to achieve our desired thrust.

●Successfully completed dry run pressurization test and cold fire test of the engine by the time I graduated.

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