Morgan Tilong
3050 Madison Ave Apt 5, Boulder, CO 80303
(720) 296-1491
tilong@colorado.edu
Objective
Seeking a part time/full time position in an aerospace engineering related field, specifically research,development and
testing. My goal is to learn about it means to work in the industry and be part of teamto utilize the skills I learned as a
student.
Work Experience: Electrical Engineering Intern at Ball Aerospace & Technologies
May-August 2015
Worked in the electrical engineering departmentat Ball Aerospace asa powerelectronics engineering aid/technician
for the ozone mapping profiler suite sensor which will be used on the Joint Polar Satellite Systems launching in 2017.
Responsibilities include, circuit design, PCB (printed circuit board) design, circuit board testing and worst case analysis
testing. Used Spice software for circuit simulations, telemetry simulation, Mentor graphics for PCB trace width power
integrity analysis, and conducted tests on satellite ground and flight circuit boards.
May-August 2016
Worked within the mission systems/tactical solutions cell to design test scripts and COSMOS GUIs to test FPGA
performance, measure processed digital signal amplitudes and define telemetry produced by FPGAs. Apply knowledge of
computer programming and architecture in designing software for anti-jamming GPS digital electronics board.
Relevant Coursework
• Statics & Structures
• Dynamics & Systems
• Aerodynamics
• Thermodynamics
• Vehicle Design &
Performance
• Applied Calculus I-III
• Differential Equations
• Orbital
Mechanics/Attitude
Determination
• Experimental Methods
• Semiconductor
Electronics
• Structures
• Circuits I-II
• Electronics Design
• Signals and Systems
• Project Management
• Aerospace Software
• Human Factors in Design
• Aircraft Dynamics
• Naval Weapons Systems
Proficiencies Technical/Non-TechnicalSkills
• MATLAB (parallel
processing)
• C/Arduino/Spice
• Microsoft office (Excel)
• COSMOS
• Proficient in AIAA formatting
Lab Experience (Design, Analysis, and Teamwork in Academia)
• Team lead for the design of frequency response analog circuit robot platform. Included the use of Spice simulations,
prototyping, and testing the necessarycircuitry to operate the robot control plate form using sound and a radio-frequency
remote controller.
• Wind Tunnel Testing and Optimization of Lockheed Martin F-16 Fighting Falcon – Incorporated LabVIEWwind tunnel
data, MATLAB, AeroDYNAMIC 3.0, and a House of Quality to model and optimize the payload, range, and fuel
consumption by optimizing altitude, aspect ratio, cruise speed,wing area,sweep angle,and taper ratio for the Lockheed
Martin F-16 at low-speed conditions.
• Design and Optimization of Truss Structure – Used MATLAB to design a single direction optimized truss structure and
model performance to determine maximum distance before failure, and assembled model using carbon fiber tuning and
magnets to test design performance.
Morgan Tilong
3050 Madison Ave Apt 5, Boulder, CO 80303
(720) 296-1491
tilong@colorado.edu
Education
University ofColorado at Boulder, Bachelor ofScience - Aerospace Engineering
GPA: 2.9 as ofSpring 2016
Graduation Date: May 2017
ď‚· Minor: Electrical Engineering (emphasis in electrical power systems, Signal and Control Systems)
ď‚· Certificate: Engineering Management (emphasis in project management)
References: James Simons: Principle Engineer, Staff Consultant, Ball Aerospace & Technologies, Boulder, CO, phone:
303-939-4116 office: email: jsimons@ball.com

Morgan Tilong Job Resume

  • 1.
    Morgan Tilong 3050 MadisonAve Apt 5, Boulder, CO 80303 (720) 296-1491 tilong@colorado.edu Objective Seeking a part time/full time position in an aerospace engineering related field, specifically research,development and testing. My goal is to learn about it means to work in the industry and be part of teamto utilize the skills I learned as a student. Work Experience: Electrical Engineering Intern at Ball Aerospace & Technologies May-August 2015 Worked in the electrical engineering departmentat Ball Aerospace asa powerelectronics engineering aid/technician for the ozone mapping profiler suite sensor which will be used on the Joint Polar Satellite Systems launching in 2017. Responsibilities include, circuit design, PCB (printed circuit board) design, circuit board testing and worst case analysis testing. Used Spice software for circuit simulations, telemetry simulation, Mentor graphics for PCB trace width power integrity analysis, and conducted tests on satellite ground and flight circuit boards. May-August 2016 Worked within the mission systems/tactical solutions cell to design test scripts and COSMOS GUIs to test FPGA performance, measure processed digital signal amplitudes and define telemetry produced by FPGAs. Apply knowledge of computer programming and architecture in designing software for anti-jamming GPS digital electronics board. Relevant Coursework • Statics & Structures • Dynamics & Systems • Aerodynamics • Thermodynamics • Vehicle Design & Performance • Applied Calculus I-III • Differential Equations • Orbital Mechanics/Attitude Determination • Experimental Methods • Semiconductor Electronics • Structures • Circuits I-II • Electronics Design • Signals and Systems • Project Management • Aerospace Software • Human Factors in Design • Aircraft Dynamics • Naval Weapons Systems Proficiencies Technical/Non-TechnicalSkills • MATLAB (parallel processing) • C/Arduino/Spice • Microsoft office (Excel) • COSMOS • Proficient in AIAA formatting Lab Experience (Design, Analysis, and Teamwork in Academia) • Team lead for the design of frequency response analog circuit robot platform. Included the use of Spice simulations, prototyping, and testing the necessarycircuitry to operate the robot control plate form using sound and a radio-frequency remote controller. • Wind Tunnel Testing and Optimization of Lockheed Martin F-16 Fighting Falcon – Incorporated LabVIEWwind tunnel data, MATLAB, AeroDYNAMIC 3.0, and a House of Quality to model and optimize the payload, range, and fuel consumption by optimizing altitude, aspect ratio, cruise speed,wing area,sweep angle,and taper ratio for the Lockheed Martin F-16 at low-speed conditions. • Design and Optimization of Truss Structure – Used MATLAB to design a single direction optimized truss structure and model performance to determine maximum distance before failure, and assembled model using carbon fiber tuning and magnets to test design performance.
  • 2.
    Morgan Tilong 3050 MadisonAve Apt 5, Boulder, CO 80303 (720) 296-1491 tilong@colorado.edu Education University ofColorado at Boulder, Bachelor ofScience - Aerospace Engineering GPA: 2.9 as ofSpring 2016 Graduation Date: May 2017 ď‚· Minor: Electrical Engineering (emphasis in electrical power systems, Signal and Control Systems) ď‚· Certificate: Engineering Management (emphasis in project management) References: James Simons: Principle Engineer, Staff Consultant, Ball Aerospace & Technologies, Boulder, CO, phone: 303-939-4116 office: email: jsimons@ball.com